Computational Fluid Dynamics Approach to Predict the Actual ... - MDPI

5 downloads 0 Views 7MB Size Report
Jun 29, 2018 - Computational Fluid Dynamics Approach to Predict the Actual Wind Speed over Complex Terrain. Takanori Uchida ID. Research Institute for ...
energies Article

Computational Fluid Dynamics Approach to Predict the Actual Wind Speed over Complex Terrain Takanori Uchida

ID

Research Institute for Applied Mechanics (RIAM), Kyushu University, 6-1 Kasuga-kouen, Kasuga, Fukuoka 816-8580, Japan; [email protected]  

Received: 24 May 2018; Accepted: 22 June 2018; Published: 29 June 2018

Abstract: This paper proposes a procedure for predicting the actual wind speed for flow over complex terrain with CFD. It converts a time-series of wind speed data acquired from field observations into a time-series data of actual scalar wind speed by using non-dimensional wind speed parameters, which are determined beforehand with the use of CFD output. The accuracy and reproducibility of the prediction procedure were investigated by simulating the flow with CFD with the use of high spatial resolution (5 m) surface elevation data for the Noma Wind Park in Kagoshima Prefecture, Japan. The errors of the predicted average monthly wind speeds relative to the observed values were less than approximately 20%. Keywords: Keywords: CFD; complex terrain; time-series data of actual scalar wind speed

1. Introduction A significant reduction in CO2 emissions to prevent global warming is currently an urgent issue. For this reason, the effective use of clean, environmentally-friendly wind energy has received attention. Since the power output of a wind turbine (WT) is proportional to the cube of the wind speed, it is extremely important to accurately select sites with wind conditions that are well suited for WT deployment with a high degree of precision. In Japan, most terrain is complex and few areas are flat, which is quite different from the terrain in Europe and the U.S. Thus, it is very important to take into account the effects of terrain on the wind flow, such as flow impingement, flow separation, flow reattachment and reverse flow. Given this background, micro-siting software, which can simulate wind over the complex terrain that is unique to Japan, is currently being developed based on computational fluid dynamics (CFD). This development is being carried out with the vision that the software can also be applied for micro-siting of WTs over complex terrain in any other part of the world [1–12]. The author’s research group has also been developing such software, specifically an unsteady, nonlinear wind simulator called RIAM-COMPACT (Research Institute for Applied Mechanics, Kyushu University, COMputational Prediction of Airflow over Complex Terrain), which is applicable for almost any flat or complex terrain across the world [13–22]. RIAM-COMPACT is based on a large-eddy simulation (LES), which is a turbulence model, and simulates airflow in small domains of approximately a few hundreds of meters to a few kilometers. One of the major features of RIAM-COMPACT is that it can, with high accuracy, predict and visualize, in the form of animation, the effects of terrain on the wind flow such as flow separation, the formation of reverse flow regions, which results from flow separation, local flow acceleration and reattachment of separated shear layers. At a planned construction site for a wind power facility, it is standard practice for an observation pole of 30 m or taller to be set up to collect time-series data of wind direction, speed and other meteorological variables over a period of one year. If these observation data can be loaded into a CFD model and both the observed data and the CFD output can be combined efficiently, economic Energies 2018, 11, 1694; doi:10.3390/en11071694

www.mdpi.com/journal/energies

Energies 2018, 11, x FOR PEER REVIEW

2 of 14

loaded into a CFD model and both the observed data and the CFD output can be combined 2 of 14 assessments of the wind power facility, including assessments of the annual energy production and capacity factor at an arbitrary location within the facility, can be made with high accuracy. assessments of the wind power facility, including assessments of the annual energy production and Accordingly, the present study proposes a procedure to predict the actual wind speed over capacity factor at an arbitrary location within the facility, can be made with high accuracy. complex terrain based on time-series data collected from field observations and CFD output. In this Accordingly, the present study proposes a procedure to predict the actual wind speed over procedure, a time-series of wind speed data acquired from field observations is converted into a complex terrain based on time-series data collected from field observations and CFD output. In this time-series of the actual scalar wind speed for the prediction point with the use of procedure, a time-series of wind speed data acquired from field observations is converted into (non-dimensional) wind speed parameters, which were determined beforehand with the use of a time-series of the actual scalar wind speed for the prediction point with the use of (non-dimensional) CFD output. The validity of the proposed procedure is examined for Noma Wind Park, Kagoshima wind speed parameters, which were determined beforehand with the use of CFD output. The validity Prefecture, Japan, with the use of observation data collected with propeller vane anemometers of the proposed procedure is examined for Noma Wind Park, Kagoshima Prefecture, Japan, with the mounted on the nacelles of WTs. use of observation data collected with propeller vane anemometers mounted on the nacelles of WTs. Energies 2018, 11, 1694 efficiently, economic

2. Overview of Noma Wind Park, Kagoshima Prefecture 2. Overview of Noma Wind Park, Kagoshima Prefecture Noma Wind Park is in Minami Satsuma City in the southwestern part of Kagoshima Noma Wind Park is in Minami Satsuma City in the southwestern part of Kagoshima Prefecture, Prefecture, Japan (marked by the circle in Figure 1). The terrain at and in the surrounding area of Japan (marked by the circle in Figure 1). The terrain at and in the surrounding area of Noma Wind Noma Wind Park is steep complex terrain (Figure 2). While the wind park is surrounded by the Park is steep complex terrain (Figure 2). While the wind park is surrounded by the ocean, a steep cliff ocean, a steep cliff with a slope angle of more than 30 degrees is at the western end of the cape. The with a slope angle of more than 30 degrees is at the western end of the cape. The maximum elevation maximum elevation of the terrain surface is 143 m. In Noma Wind Park, ten WTs that are owned by of the terrain surface is 143 m. In Noma Wind Park, ten WTs that are owned by Kyushu Electric Power Kyushu Electric Power Co., Inc. (Fukuoka, Japan), have been deployed, and verification tests have Co., Inc. (Fukuoka,The Japan), beenofdeployed, verification have rated been conducted. been conducted. ratedhave output each WT and is 300 kW; thus,tests the total output fromThe therated ten output of each WT is 300 kW; thus, the total rated output from the ten WTs combined is 3000 kW. WTs combined is 3000 kW. Tables 1 and 2 give an overview of the WTs deployed in Noma Wind Tables 1 and 2 give an overview of the WTs deployed in Noma Wind Park. Park.

Figure 1. Cape Noma and surrounding topographical features. Figure 1. Cape Noma and surrounding topographical features.

Energies 2018, 11, 1694

3 of 14

Energies 2018, 11, x FOR PEER REVIEW

3 of 14

Figure 2. View of Noma Wind Park. Table (WTs) at at Noma Noma Wind Wind Park. Park. Table 1. Specifications of wind turbines (WTs)

Item WT #1–#5 WT #6–#10 WT #1–#5 WT #6–#10 Output 300 kW/WT Output 300 kW/WT Generator type Induction Synchronous Generator type Induction Synchronous Cut-in speed 3.5 m/s 2.5 m/s2.5 m/s Cut-in speed 3.5 m/s Rated wind speed 14.4 14.4 m/s 14.0 m/s14.0 m/s Rated wind speed m/s Cut-out speed 24 24 m/s Cut-out speed m/s 25 m/s 25 m/s Rotor diameter 29 m Rotor diameter 29 m 30 m 30 m 30 m 30 m Tower height 30 m 30 m (WT #4:45 m) (WT #6:45 m) Tower height (WT #4:45 m) (WT #6:45 m) Item

Table 2. WT hub-heights and surface elevations.

Number WT #1 WT #2 WT #3

Hub-Height (Tower Height) 30 m

Surface Elevation of WT Site 100 m 92 m 109 m

Energies 2018, 11, 1694

4 of 14

Table 2. WT hub-heights and surface elevations. Energies FOR Energies2018, 2018,11, 11,xxNumber FORPEER PEERREVIEW REVIEW Hub-Height (Tower Height)

WT #1 WT#4 #2 WT WT #4 WT#5 #3 WT WT #5 WT #4 WT #6 WT WT #6 #5 WT #7 WT WT #7 #6 WT#8 #7 WT WT #8 WT #8 WT WT #9 #9 WT #9 WT #10 WT WT #10 #10

45 45 m m 30 m 30 m 30 m 45 m 45 45 m m 30 m 45 m

30 30 m m

30 m

Surface Elevation of WT Site

44of of14 14

100 m 122 122 m m92 m 109 m 102 102 m m 122 m 117 117 m m102 m 88 88 m m117 m 95 95 m m 88 m 92 92 m m 95 m 92 m 109 109 m m109 m

Propeller Propeller vane vane anemometers anemometers are are mounted mounted on on all all of of the the WTs WTs deployed deployed in in Noma Noma Wind Wind Park Park Propeller vane anemometers are mounted on all of the WTs deployed in Noma Wind Park (indicated by “A” in Figure 3). The present study employs time-series observation data from these (indicated by “A” in Figure 3). The present study employs time-series observation data from these (indicated by “A” in Figure 3). The The study employsevery time-series observation data propeller anemometers. data recorded one Details of the wind propeller vane vane anemometers. The present data were were recorded every one minute. minute. Details offrom the these wind propeller vane anemometers. The data were recorded every one minute. Details of the wind characteristics characteristics at at Noma Noma Wind Wind Park Park from from June June 2002–May 2002–May 2003 2003 are are summarized summarized in in Uchida. Uchida. According According characteristics Noma Wind Parkdirection from June 2003 are summarized Uchida.average According to to wind at this northerly, and monthly wind to Uchida, Uchida, the theatprevailing prevailing wind direction at2002–May this site site is is northerly, and the the in monthly average wind Uchida, the prevailing wind direction at this site is northerly, and the monthly average wind speed speed speed is is large large from from November–March November–March (see (see Figures Figures 44 and and 5). 5). The The present present study study validates validates the the is large from November–March (seethe Figures and 5). Thewith present the data proposed proposed procedure for actual speed the use observation from proposed procedure for predicting predicting the actual4wind wind speed with the study use of ofvalidates observation data from procedure for predicting the actualthe wind speed with the use observation data from February 2003, February the during observation period in which the data are all February 2003, 2003, the month month during the observation period inof which the least least data are missing missing for for all the month during the observation period in which the least data are missing for all ten WTs and also in ten ten WTs WTs and and also also in in which which the the value value of of the the monthly monthly average average wind wind speed speed is is large. large. For For February February 2003, 2003, which value the values monthly average wind speed is large. February 2003, 40,047 and 273 data 40,047 and 273 data available for analysis and missing, respectively (percentage of 40,047the and 273 of data values are are available for analysis andFor missing, respectively (percentage of values are available for analysis and missing, respectively (percentage of non-missing data: 99%). non-missing non-missing data: data: 99%). 99%).

Figure nacelle (indicated by “A”). Figure3. 3.Propeller Propellervane vaneanemometer anemometermounted mountedon onaaaWT WTnacelle nacelle(indicated (indicatedby by“A”). “A”). Figure 3. Propeller vane anemometer mounted on WT

(a) (a)

(b) (b)

Figure Figure4. 4.Characteristics Characteristicsof ofwind windat atNoma NomaWind WindPark, Park,WT WT#4, #4,for forthe theyear yearfrom fromJune June2002–May 2002–May2003. 2003. Figure 4. Characteristics of wind at Noma Wind Park, WT #4, for the year from June 2002–May 2003. (a) (a)Occurrence Occurrencefrequency frequency(%); (%);(b) (b)annual annualaverage averagewind windspeed speed(m/s). (m/s). (a) Occurrence frequency (%); (b) annual average wind speed (m/s).

Energies 2018, 11, 1694 Energies 2018, 11, x FOR PEER REVIEW

5 of 14 5 of 14

(a)

(b)

Figure 5. Characteristics of wind at Noma Wind Park, WT #4, for the month of February 2003. Figure 5. Characteristics of wind at Noma Wind Park, WT #4, for the month of February 2003. (a) Occurrence frequency (%); (b) monthly average wind speed (m/s). (a) Occurrence frequency (%); (b) monthly average wind speed (m/s).

3. Numerical Simulation Technique and Set-up 3. Numerical Simulation Technique and Set-up The present study employs the wind farm design tool called RIAM-COMPACT. This software The present study employs the wind farm design tool called RIAM-COMPACT. This software simulates neutral wind flow with the use of a collocated grid arrangement in a general curvilinear simulates neutral wind flow with the use of a collocated grid arrangement in a general curvilinear coordinate system. For the governing equations of the flow, a filtered continuity equation for coordinate system. For the governing equations of the flow, a filtered continuity equation for incompressible fluid (Equation (1)) and filtered Navier–Stokes equations (Equation (2)) are used. incompressible fluid (Equation (1)) and filtered Navier–Stokes equations (Equation (2)) are used. The effects of the surface roughness have been taken into consideration by reconstructing surface The effects of the surface roughness have been taken into consideration by reconstructing surface irregularities at high resolution (horizontal spatial resolution: 5 m). irregularities at high resolution (horizontal spatial resolution: 5 m). ∂u i (1) ∂ui = 0 ∂xi = 0 (1) ∂xi ∂ p 11 ∂∂22uui i ∂τ∂τ ij ∂ui∂ui + u∂u∂i ui = −∂p + −− ij (2) + uj j = − + (2) t x x Re x x x ∂ ∂ ∂ ∂ ∂ ∂ ∂t ∂x j j ∂xii Re ∂xj j ∂xj j ∂x j j 1 ' 0 ' ≈ 1u 0' u 0' δ − 2ν τijτ ij≈≈uui0 u u ≈ u u δ − 2ν SGS SGSSSijij j i j 33 kk kk ijij νSGS = (Cs f s ∆)22 S ν = ( Cs f s Δ ) S SGS  S = 2Sij Sij 1/2 1/ 2 ! S = 2Sij Sij ∂u j 1 ∂ui Sij = + 21 ∂x u ji  ∂uji ∂∂x + Sij =    ∂x j +  i  f s = 1 −2exp  −z ∂x/25 1/3 hzz + / 25 f∆ 1 − hexp x hy − s ==

(

)

(

)

(3) (3) (4) (4) (5) (5) (6)

(6) (7) (8) (7)

For the computational algorithm, a fractional step (FS) method [23] is used. A time marching method 1/ 3 Δ = hx hy hz (8) based on the Euler explicit method is adopted. Poisson’s equation for pressure is solved by a successive over-relaxation (SOR) method. For discrimination of all the spatial terms in the governing equations For the computational algorithm, a fractional step (FS) method [23] is used. A time marching except for the convective term in Equation (2), a second-order central difference scheme is applied. method based on the Euler explicit method is adopted. Poisson’s equation for pressure is solved by For the convective term, a third-order upwind difference scheme is used. For the fourth-order a successive over-relaxation (SOR) method. For discrimination of all the spatial terms in the central difference term that constitutes the discretized convective term, the interpolation technique governing equations except for the convective term in Equation (2), a second-order central of Kajishima [24], which is based on a four-point difference scheme and a four-point interpolation difference scheme is applied. For the convective term, a third-order upwind difference scheme is scheme, is used. For the weighting of the numerical diffusion term in the discretized convective term, used. For the fourth-order central difference term that constitutes the discretized convective term, α = 3.0 is commonly applied in the Kawamura–Kuwahara scheme [25]. However, α = 0.5 is used in the the interpolation technique of Kajishima [24], which is based on a four-point difference scheme and present study to minimize the influence of numerical diffusion. For the LES subgrid-scale modeling, a four-point interpolation scheme, is used. For the weighting of the numerical diffusion term in the the standard Smagorinsky model [26] (Equations (3)–(8)) is adopted with a model coefficient of 0.1 in discretized convective term, α = 3.0 is commonly applied in the Kawamura–Kuwahara scheme [25]. conjunction with a wall-damping function. However, α = 0.5 is used in the present study to minimize the influence of numerical diffusion. For

(

)

Energies 2018, 11, x FOR PEER REVIEW

6 of 14

the LES2018, subgrid-scale modeling, the standard Smagorinsky model [26] (Equations (3)–(8)) Energies 11, 1694 6 ofis 14 adopted with a model coefficient of 0.1 in conjunction with a wall-damping function. Procedurefor forPredicting PredictingActual ActualWind WindSpeed Speed 4.4.Procedure The procedure procedure for wind speed time-series datadata for an point The for predicting predictingthe theactual actualscalar scalar wind speed time-series forarbitrary an arbitrary in complex terrain is described as follows. In this procedure, time-series data that were acquired from point in complex terrain is described as follows. In this procedure, time-series data that were field observations CFD output (time-averaged wind speed) are utilized. acquired from fieldand observations and CFD output (time-averaged wind speed) are utilized. Step 1. As Figure 6, wind patterns are simulated by RIAM-COMPACT for 16 individual Step Asshown shownin in Figure 6, wind patterns are simulated by RIAM-COMPACT for 16 wind directions for a prediction point. After the flow field has fully developed in a simulation individual wind directions for a prediction point. After the flow field has fully developed inrun, a the simulation continued, and the time-averaged is calculated. simulation run, is the simulation is continued, and the flow time-averaged flow is calculated.

Figure Figure6.6.Conceptual Conceptualoutline outlineofofwind windsimulations simulationsfor for16 16wind winddirections directionsfor forNoma NomaWind WindPark. Park.

The computational domain is a square with 5 km sides with WT #4 in the center of the domain The computational domain is a square with 5 km sides with WT #4 in the center of the domain (Figure 6). The top boundary of the computational domain is set to 700 m. Terrain features are (Figure 6). The top boundary of the computational domain is set to 700 m. Terrain features are reconstructed with the use of high-resolution (5 m horizontal spatial resolution) surface elevation reconstructed with the use of high-resolution (5 m horizontal spatial resolution) surface elevation data. data. The numbers of computational grid cells are 51 (streamwise (x)) × 51 (spanwise (y)) × 41 The numbers of computational grid cells are 51 (streamwise (x)) × 51 (spanwise (y)) × 41 (vertical (z)). (vertical (z)). Variable grid pacing is used in the x- and y-directions so that the grid density increases Variable grid pacing is used in the x- and y-directions so that the grid density increases toward the toward the center of the domain. Likewise, variable grid spacing is used in the z-direction so that center of the domain. Likewise, variable grid spacing is used in the z-direction so that grid density is grid density is highest near the ground surface. The vertical height of the first layer of grid cells, highest near the ground surface. The vertical height of the first layer of grid cells, that is the minimum that is the minimum vertical grid height, is approximately 2.5 m. A vertical profile of wind speed vertical grid height, is approximately 2.5 m. A vertical profile of wind speed based on the 1/7 power based on the 1/7 power law is given for the inflow boundary. The free-slip condition is set for the law is given for the inflow boundary. The free-slip condition is set for the side and upper boundaries. side and upper boundaries. The convective outflow condition is applied to the outflow boundary. The convective outflow condition is applied to the outflow boundary. On the ground, the no-slip On the ground, the no-slip condition is imposed. The non-dimensional parameter, Re, in Equation condition is imposed. The non-dimensional parameter, Re, in Equation (2), defined as Uin h/ν, (2), defined as Uin h/ν, is the Reynolds4 number and is set to 104. Here, h indicates the difference is the Reynolds number and is set to 10 . Here, h indicates the difference between the minimum and between the minimum and maximum surface elevations within the computational domain (h = 143 maximum surface elevations within the computational domain (h = 143 m). Uin represents the wind m). Uin represents the wind speed at the inflow boundary at the height of the maximum surface speed at the inflow boundary at the height of the maximum surface elevation in the computational elevation in the computational domain, and ν is the coefficient of kinematic viscosity. The domain, and ν is the coefficient of kinematic viscosity. The representative scales used for the present representative scales used for the present simulations, h and Uin, are shown in Figure 7. The time simulations, h and Uin , are shown in−3Figure 7. The time step in the model is set to ∆t = 2 × 10−3 h/Uin . step in the model is set to ∆t = 2 × 10 h/Uin.

Energies 2018, 11, 1694 Energies 2018, 11, x FOR PEER REVIEW

7 of 14 7 of 14

Figure Figure 7. 7. Representative Representative scales scales used usedin inthe thepresent presentstudy. study.

Step2.2.For For each each inflow inflow direction direction (Figure at (Figure 6), 6), the theratio ratioof ofthe thesimulated simulatedhub-height hub-heightwind windspeed speed Step a prediction point to the simulated wind speed at the height of an observation pole, that is, at the at a prediction point to the simulated wind speed at the height of an observation pole, that is, at the referencepoint, point,isiscomputed, computed, yielding a set ofwind 16 wind speed forprediction the prediction The reference yielding a set of 16 speed ratiosratios for the point. point. The value value of the wind speed at the reference point is normalized as “1”. In this step, the wind direction of the wind speed at the reference point is normalized as “1”. In this step, the wind direction set at the set at the inflowisboundary that at the reference point. In the points presentlocated study, inflow boundary assumed is to assumed match thattoatmatch the reference point. In the present study, points located at WT #4the andhub-height WT #6 at the used aspoints the reference points (hereafter, in at WT #4 and WT #6 at are hub-height used as theare reference (hereafter, in the context of the context of reference points, these reference points will be referred to as WT #4 and WT #6). reference points, these reference points will be referred to as WT #4 and WT #6). Thus, the following Thus,speed the following speedWT ratios are evaluated: #1/WT#4; #4,WT …,#1/WT WT #10/WT WT #1/WT wind ratios are wind evaluated: #1/WT #4, . . . , WTWT #10/WT #6, . . . #4; , WT #10/WT #6, …, WT #10/WT #6. To compute these wind speed ratios, the scalar wind speed, VEL, is used in #6. To compute these wind speed ratios, the scalar wind speed, VEL, is used in both the denominator both the denominator and numerator and is computed from the time-averaged wind velocity and numerator and is computed from the time-averaged wind velocity components in the x- and components Here, in thethe x- and y-directions. thetophysical quantity to as VEL is defined as y-directions. physical quantity Here, referred as VEL is definedreferred as follows: follows: q VEL =

2

2

(U + V )

VEL = (U 2 + V 2 )

(9) (9)

Step Step3.3.The Theobserved observedtime-series time-seriesof ofthe thescalar scalarwind windspeed speedat atthe thereference referencepoint pointisisconverted convertedto to aatime-series of scalar wind speed at a prediction point as follows. According to the wind time-series of scalar wind speed at a prediction point as follows. According to the winddirection direction at at the the reference reference point pointat ataagiven giveninstance instancein inthe theobserved observedtime-series, time-series, the the scalar scalar wind wind speed speed at at the the reference point is multiplied by the wind speed ratio, which was determined beforehand for reference point is multiplied by the wind speed ratio, which was determined beforehand for the the prediction forfor thatthat wind direction in Step By applying this operation to an observed predictionpoint point wind direction in2.Step 2. By applying this operation to antime-series observed of scalar wind speeds that extends over a period of one year or any period of interest and processing time-series of scalar wind speeds that extends over a period of one year or any period of interest the of the operation the monthly and annual be obtained andoutcome processing the outcomestatistically, of the operation statistically, the average monthlywind and speed annualcan average wind for an arbitrary prediction point. speed can be obtained for an arbitrary prediction point. 5. Results and Discussion 5. Results and Discussion Figure 8 illustrates instantaneous views of flows that were visualized with the passive particle Figure 8 illustrates instantaneous views of flows that were visualized with the passive particle tracking method. The inflow wind direction for this case is northerly. This figure indicates that, tracking method. The inflow wind direction for this case is northerly. This figure indicates that, due due to the influence of the terrain irregularities, wind speed and direction change in complex ways to the influence of the terrain irregularities, wind speed and direction change in complex ways as as the wind flows over Cape Noma. In the procedure for predicting the actual wind speed that is the wind flows over Cape Noma. In the procedure for predicting the actual wind speed that is proposed in the present study, simulations are run until fully-developed flows, as the one illustrated in proposed in the present study, simulations are run until fully-developed flows, as the one Figure 8, are achieved, and the simulations are continued for a period of time. Then, the results of the illustrated in Figure 8, are achieved, and the simulations are continued for a period of time. Then, simulations are used to obtain the time-averaged flow field. the results of the simulations are used to obtain the time-averaged flow field.

Energies 2018, 11, 1694

8 of 14

Energies 2018, 11, x FOR PEER REVIEW Energies 2018, 11, x FOR PEER REVIEW

8 of 14 8 of 14

Flow Flow

Figure 8. Examples of flows visualized with thethe passive particle tracking method, northerly wind, Figure 8. Examples of flows visualized with passive particle tracking method, northerly wind, Figure 8. Examples of flows visualized with the passive particle tracking method, northerly wind, bird’s eyeeye view. bird’s view. bird’s eye view.

Figureshows 9 shows comparisonsofofthe theobserved observedand andpredicted predicted time-series time-series of scalar wind speed for Figure comparisons scalar wind speed Figure 99 shows comparisons of the observed and predicted time-series of of scalar wind speed for the hub-height ofofWT #1#1and WT #10. ToToobtain the scalar wind speed inin this figure, WT for hub-height WT and obtain thepredicted predicted scalar speed this figure, the the hub-height of WT #1 and WT WT #10.#10. To obtain the predicted scalar windwind speed in this figure, WT #4 was used as the reference point. Figure 10 shows scatter plots of the observed and predicted WT #4 was used as the reference point. Figure showsscatter scatterplots plotsofofthe the observed observed and and predicted #4 was used as the reference point. Figure 1010shows predicted scalar wind speed from Figure 9. Figure 11 also shows comparisons of the observed and predicted scalar scalar wind wind speed speed from from Figure Figure 9. 9. Figure Figure 11 11 also also shows shows comparisons comparisons of of the the observed observed and and predicted predicted time-series of scalar wind speed forhub-height the hub-height of#1WT #1WT and WT #10; however, WT used #6 was time-series of scalar wind speed for the of WT and #10; however, WT #6 was time-series of scalar wind speed for the hub-height of WT #1 and WT #10; however, WT #6 was used as the reference point for the prediction of the scalar wind speed. Scatter plots for the data in as theas reference point for the for prediction of the scalar speed. for plots the data Figure used the reference point the prediction of thewind scalar windScatter speed.plots Scatter forin the data 11 in Figure 11 shown In in both Figure In of both theWT case ofand using WT #4 the case WT #6 as are shown inare Figure the12. case the of and using WT #6 of as using the WT reference Figure 11 are shown12. in Figure 12. In both using the case of#4using WTcase #4 and the case of using #6 as the reference points, the proposed procedure for predicting the actual wind speed yielded points, the proposed for predicting the for actual wind speed values that the reference points,procedure the proposed procedure predicting the yielded actual predicted wind speed yielded predicted values that agree well with the observed values. agree well with the observed values. predicted values that agree well with the observed values.

(a) WT #1 (a) WT #1

(b) WT #10 (b) WT #10

Figure 9. Time-series data of observed and predicted wind speed, reference point: WT #4. Figure 9. Time-series data of observed and predicted wind speed, reference point: WT #4. Figure 9. Time-series data of observed and predicted wind speed, reference point: WT #4.

Energies 2018, 11, 1694 Energies 2018, 11, x FOR PEER REVIEW

9 of 14 9 of 14

Energies 2018, 11, x FOR PEER REVIEW Energies 2018, 11, x FOR PEER REVIEW

9 of 14 9 of 14

(a) WT #1 (b) WT #10 (a) WT #1 (b) WT #10 (a) WTof #1 (b) WT #10 point: WT #4. Figure 10. 10. Scatter and predicted predicted wind wind speed, speed, reference Figure Scatter plots plots of observed observed and reference point: WT #4. Figure 10. Scatter plots of observed and predicted wind speed, reference point: WT #4. Figure 10. Scatter plots of observed and predicted wind speed, reference point: WT #4.

(a) (a)WT WT#1#1 (a) WT #1

(b)WT WT#10 #10 (b) (b) WT #10

Figure 11.11. Time-series windspeed, speed,reference referencepoint: point: WT Figure Time-seriesdata dataof ofobserved observed and predicted predicted wind WT #6.#6. Figure 11.11. Time-series wind speed, speed,reference referencepoint: point:WT WT Figure Time-seriesdata dataofofobserved observed and and predicted predicted wind #6.#6.

(a) WT #1 (a)WT WT#1 #1 (a)

(b) WT #10 (b) (b)WT WT#10 #10

Figure 12. Scatter plots of observed and predicted wind speed, reference point: WT #6. Figure Scatter plotsofofobserved observed and and predicted predicted wind WT #6.#6. Figure 12.12. Scatter windspeed, speed,reference referencepoint: point: WT Figure 12. Scatter plots plots of observed and predicted wind speed, reference point: WT #6.

Table 3 summarizes the comparisons of observed and predicted values of wind speed for the Table 3 summarizes thecomparisons comparisons of observed and values forfor thethe Table 3 summarizes observed and predicted predicted values ofwind windspeed speed cases of adopting WT #4the and WT #6 as theof reference points. Table 4 gives the of horizontal separation Table 3adopting summarizes theand comparisons of observed and predicted values of wind speed separation for the cases cases of WT #4 WT #6 as the reference points. Table 4 gives the horizontal distance betweenWT a given WT and #4 or WT #6, points. both of Table which4were as referenceseparation points. cases of adopting #4 and WT #6WT as the reference givesused the horizontal of adopting WT #4 and WT #6 asand the WT reference Table 4 gives the horizontal separationpoints. distance distance between given WT #4difference or points. WT #6, #6,between both were Similarly, Table a5agiven shows theand elevation the hub-height ofasas areference given WT points. and distance between WT WT #4 or WT both of of which which wereused used reference between a given and WT or Examinations WT #6,difference both of which were used as reference Similarly, Similarly, TableWT 5 shows the#4#6. elevation between hub-height a points. given WT reference point #4 or the WT of Tables 3–5the reveal that the of relative error of and the Similarly, Table 5WT shows elevation difference between the hub-height of a given WT and Table 5 shows the elevation difference betweenactual the hub-height ofprediction a given WT and reference point reference point WT #4 or WT #6.the Examinations of Tables 3–5 reveal that the relative error ofthan the wind speed at a WT predicted by proposed wind speed procedure is less reference point WT #4 or WT #6. Examinations of Tables 3–5 reveal that the relative error of the wind speed at a20% WT predicted by the proposed actual wind speed prediction difference procedure between is less than approximately if the horizontal separation distance and elevation a wind speed at a WT predicted by the proposed actual wind speed prediction procedure is less than approximately 20% if the horizontal separation distance and elevation difference between a

approximately 20% if the horizontal separation distance and elevation difference between a

Energies 2018, 11, 1694

10 of 14

WT #4 or WT #6. Examinations of Tables 3–5 reveal that the relative error of the wind speed at a WT predicted by the proposed actual wind speed prediction procedure is less than approximately 20% if the horizontal separation distance and elevation difference between a prediction point (the hub-height of a WT) and the reference point are approximately 800 m or less and 50 m or less, respectively. As expected, the observed wind speed data that are used in the present study were affected by the blade rotation since they were collected from propeller vane anemometers that were mounted on the nacelles of the WTs. However, this effect is equally present in the wind speed data that were collected at all the WTs. Table 3. Comparisons of observed and predicted values of wind speed. (a) Reference Point: WT #4 February 2003

Observed Wind Speed (m/s)

Predicted Wind Speed (m/s)

Relative Error (%)

Correlation Coefficient

WT #1 WT #2 WT #3 WT #5 WT #6 WT #7 WT #8 WT #9 WT #10 Average

7.27 7.07 7.91 7.11 7.39 6.35 6.78 6.17 6.57 6.96

7.45 7.24 7.60 7.45 7.83 7.06 7.40 7.20 7.41 7.40

2.56 2.31 3.92 4.84 5.90 11.28 9.09 16.62 12.84 6.42

0.90 0.89 0.93 0.91 0.92 0.83 0.90 0.84 0.86 0.89

(b) Reference Point: WT #6 February 2003

Observed Wind Speed (m/s)

Predicted Wind Speed (m/s)

Relative Error (%)

Correlation Coefficient

WT #1 WT #2 WT #3 WT #5 WT #6 WT #7 WT #8 WT #9 WT #10 Average

7.27 7.07 7.91 7.11 7.39 6.35 6.78 6.17 6.57 6.96

6.63 6.32 6.48 7.73 7.07 6.80 7.02 6.80 6.90 6.86

8.74 10.71 18.09 6.80 0.54 7.10 3.58 10.22 5.13 2.73

0.90 0.87 0.92 0.92 0.92 0.92 0.96 0.92 0.93 0.92

Table 4. Horizontal separation distance between a given WT and the reference point. Reference Point: WT #4 WT #1–WT #4 WT #2–WT #4 WT #3–WT #4 WT #5–WT #4 WT #6–WT #4 WT #7–WT #4 WT #8–WT #4 WT #9–WT #4 WT #10–WT #4

Horizontal Separation Distance (m) approx. approx. approx. approx. approx. approx. approx. approx. approx.

560 280 140 180 300 420 430 630 800

Reference Point: WT #6 WT #1–WT #6 WT #2–WT #6 WT #3–WT #6 WT #4–WT #6 WT #5–WT #6 WT #7–WT #6 WT #8–WT #6 WT #9–WT #6 WT #10–WT #6

Horizontal Separation Distance (m) approx. approx. approx. approx. approx. approx. approx. approx. approx.

760 530 350 300 140 140 240 350 500

Table 5. Elevation difference between the hub-height of a given WT (a prediction point) and the reference point. Reference Point: WT #4

Elevation Difference (m)

Reference Point: WT #6

Elevation Difference (m)

WT #1–WT #4 WT #2–WT #4 WT #3–WT #4 WT #5–WT #4 WT #6–WT #4 WT #7–WT #4 WT #8–WT #4 WT #9–WT #4 WT #10–WT #4

37 45 28 35 5 49 42 45 28

WT #1–WT #6 WT #2–WT #6 WT #3–WT #6 WT #4–WT #6 WT #5–WT #6 WT #7–WT #6 WT #8–WT #6 WT #9–WT #6 WT #10–WT #6

32 40 23 5 30 44 37 40 23

WT #5–WT #4 WT #6–WT #4 WT #7–WT #4 WT #8–WT #4 Energies WT 2018,#9–WT 11, 1694#4 WT #10–WT #4

35 5 49 42 45 28

WT #4–WT #6 WT #5–WT #6 WT #7–WT #6 WT #8–WT #6 WT #9–WT #6 WT #10–WT #6

5 30 44 37 40 23

11 of 14

In regards regards to tothe thepreviously previously discussed range of application forproposed the proposed wind discussed range of application for the actualactual wind speed speed prediction procedure, the subsequent analysis examines, based on the observation prediction procedure, the subsequent analysis examines, based on the observation data,data, the the characteristics of airflow over complex terrain, whichserve serveasassupporting supportingevidence evidencefor for the the range of characteristics of airflow over complex terrain, which application for 1313 shows a comparison of the of theofobserved wind forthe theprocedure. procedure.Figure Figure shows a comparison of time-series the time-series the observed speed from WT #1 and WT #10 and also a scatter plot of the observed wind speed from the two WTs for wind speed from WT #1 and WT #10 and also a scatter plot of the observed wind speed from the February The horizontal separation distance between the two WTs isthe as much as approximately two WTs 2003. for February 2003. The horizontal separation distance between two WTs is as much as 1200 m, and the 1200 elevation difference between the two WTs is 9 mthe (see Figure particular, attention approximately m, and the elevation difference between two WTs2). is In 9m (see Figure 2). In should be given to the should horizontal Even though the horizontal distance particular, attention be separation given to distance. the horizontal separation distance. separation Even though the between WT #1 and WT #10 is more thanWT 1000#1 m,and the temporal of the1000 wind over the horizontal separation distance between WT #10 ischanges more than m,speed the temporal course one WT #1 andthe WT #10 are similar.atThe between the changesofof themonth wind at speed over course of quite one month WTcorrelation #1 and WTcoefficient #10 are quite similar. two plotted in Figure 13b isthe 0.84. The datasets correlation coefficient between two datasets plotted in Figure 13b is 0.84.

Energies 2018, 11, x FOR PEER REVIEW

(a) Time-series data

12 of 14

(b) Scatter plot Figure 13. Comparison of hub-height wind speed at WT #1 and WT #10, observation data. Figure 13. Comparison of hub-height wind speed at WT #1 and WT #10, observation data.

Of the 40,047 values of the ratio of the wind speed at WT #1 (the prediction point) to the wind speed at WT #4 (the reference point) for February 2003, data values only from the time of northerly wind are extracted in order to study the statistical properties of the wind speed ratio. The number of extracted data values is 9501, which corresponds to approximately 24% of the entire set of data values. In this analysis, an angle of 0° denotes wind that blows from north to south, and wind that flows from wind directions that are 348.75° or larger and 11.25°or smaller are defined as northerly wind. Figure 14 shows the time-series of the wind speed ratio only for times of northerly wind.

(b) Scatter plot Figure2018, 13. Comparison of hub-height wind speed at WT #1 and WT #10, observation data. Energies 11, 1694

12 of 14

Of the 40,047 values of the ratio of the wind speed at WT #1 (the prediction point) to the wind Of (the the 40,047 values of the ratio of the wind speed at WT #1from (the the prediction to the wind speed at WT #4 reference point) for February 2003, data values only time of point) northerly speed at WT #4 (the reference point) for February 2003, data values only from the time of wind are extracted in order to study the statistical properties of the wind speed ratio. The numbernortherly winddata are values extracted in order to study the statistical properties of24% the wind number of of extracted is 9501, which corresponds to approximately of thespeed entireratio. set ofThe data extracted data values is 9501, which corresponds to approximately 24% of the entire set of data values. In this analysis, an angle of 0° denotes wind that blows from north to south, and wind that values. ◦ denotes wind that blows from north to south, and wind that flows from In this analysis, an angle of 0348.75° flows from wind directions that are or larger and 11.25°or smaller are defined as northerly ◦ wind 14 directions are 348.75◦ or and 11.25 smaller wind. Figure shows that the time-series of larger the wind speedor ratio onlyare fordefined times as of northerly northerlywind. wind.Figure 14 shows the time-series of the wind speed ratio only for times of northerly wind. Figure also shows Figure 14 also shows the average value of the observed wind speed ratios for northerly wind14and average value ofrevealing the observed ratios for northerly and Figure that from CFD model, that fromthe the CFD model, that wind these speed two average values agreewind closely. 15 the shows revealing that these two average values agree closely. Figure 15 shows the frequency distribution of the frequency distribution of the wind speed ratios plotted in Figure 14. The frequency is the wind speed ratios plotted in Figure 14. The frequency is distributed nearly symmetrically with distributed nearly symmetrically with the average wind speed ratio in the center. Thus, it can be average data windofspeed inspeed the center. it can be said that time-series of scalar said thatthe time-series scalarratio wind at an Thus, arbitrary point can be obtained withdata the use of wind speed at an arbitrary point can be obtained with the use of observed time-series of wind speed from observed time-series of wind speed from the reference point if, with the use of CFD, the effects of the reference point if, with the use of CFD, the effects of terrain irregularities on the wind flow can be terrain irregularities on the wind flow can be simulated accurately and the ratio of the wind speed simulated point accurately andwind the ratio of the windreference speed at point the prediction point to thewith windhigh speed at the at the prediction to the speed at the can be estimated reference point can be estimated with high accuracy. accuracy.

0.92 (Observed value) 0.89 (Predicted value)

14. Observed of the hub-height wind speed atthat WT at #1WT to that Figure 14.Figure Observed time-seriestime-series of the ratioofofthe theratio hub-height wind speed at WT #1 to #4, at WT #4, only for times of northerly wind, February 2003. 2018, 11, x FOR PEER 13 of 14 onlyEnergies for times of northerly wind,REVIEW February 2003.

Figure 15. 15. Frequency Frequency distribution distribution of of the the ratio ratio of of the the hub-height hub-height wind to that that at at WT WT #4, #4, Figure wind speed speed at at WT WT #1 #1 to only for times of northerly wind, February 2003. only for times of northerly wind, February 2003.

6. Conclusions In the present study, a procedure for predicting the actual wind speed over complex terrain was proposed. This procedure utilizes both time-series of observation data and CFD output obtained from the unsteady, nonlinear wind simulator RIAM-COMPACT, in which a collocated grid in a general curvilinear coordinate system is adopted. In this procedure, time-series of scalar wind speed obtained from field observations are converted to the actual scalar wind speed with the use of (non-dimensional) wind speed parameters that were obtained beforehand with the use of the CFD. The proposed prediction procedure was validated with the use of observation data acquired

Energies 2018, 11, 1694

13 of 14

6. Conclusions In the present study, a procedure for predicting the actual wind speed over complex terrain was proposed. This procedure utilizes both time-series of observation data and CFD output obtained from the unsteady, nonlinear wind simulator RIAM-COMPACT, in which a collocated grid in a general curvilinear coordinate system is adopted. In this procedure, time-series of scalar wind speed obtained from field observations are converted to the actual scalar wind speed with the use of (non-dimensional) wind speed parameters that were obtained beforehand with the use of the CFD. The proposed prediction procedure was validated with the use of observation data acquired with anemometers mounted on the nacelles of wind turbines in Noma Wind Park, Kagoshima Prefecture, Japan. As for the result, the following was found for Noma Wind Park, which was investigated in the present study. If the horizontal separation distance between a prediction point and the reference point is approximately 800 m or less and the elevation difference between the two locations is 50 m or less, the relative error of the wind speed predicted by the proposed wind speed prediction procedure is less than approximately 20%. However, additional validation is necessary in regards to how the reference location is selected and the types of observation instruments used at the reference point. In addition, validation also needs to be carried out at other sites. These validations will be topics of future research. Finally, if the proposed procedure is further expanded so that it utilizes output from a meteorological model instead of observation data, a so-called real-time forecasting, which can predict wind flows a few hours to a few days into the future, will be made possible. Funding: This research was supported by JSPS KAKENHI Grant Number 17H02053. Acknowledgments: For conducting this research, the author was provided with the various types of data on the Noma Wind Park, Kagoshima Prefecture, Japan, by Kyushu Electric Power Co., Inc. The author would like to express his gratitude to all the organizations. Conflicts of Interest: The author declares no conflict of interest.

References 1.

2. 3. 4.

5. 6. 7. 8. 9. 10.

Palma, J.M.L.M.; Castro, F.A.; Ribeiro, L.F.; Rodrigues, A.H.; Pinto, A.P. Linear and nonlinear models in wind resource assessment and wind turbine micro-siting in complex terrain. J. Wind Eng. Ind. Aerodyn. 2008, 96, 2308–2326. [CrossRef] Berg, J.; Mann, J.; Bechmann, A.; Courtney, M.S.; Jørgensen, H.E. The Bolund experiment, part I: Flow over a steep, three-dimensional hill. Bound.-Layer Meteorol. 2011, 141, 219–243. [CrossRef] Bechmann, A.; Sørensen, N.N.; Berg, J.; Mann, J.; Réthoré, P.-E. The Bolund experiment, part II: Blind comparison of microscale flow models. Bound.-Layer Meteorol. 2011, 141, 245–271. [CrossRef] Prospathopoulos, J.M.; Politis, E.S.; Chaviaropoulos, P.K. Application of a 3D RANS solver on the complex hill of Bolund and assessment of the wind flow predictions. J. Wind Eng. Ind. Aerodyn. 2012, 107, 149–159. [CrossRef] Diebold, M.; Higgins, C.; Fang, J.; Bechmann, A.; Parlange, M.B. Flow over hills: A large-eddy simulation of the Bolund case. Bound.-Layer Meteorol. 2013, 148, 177–194. [CrossRef] Porté-Agel, F.; Wu, Y.-T.; Chen, C.-H. A Numerical Study of the Effects of Wind Direction on Turbine Wakes and Power Losses in a Large Wind Farm. Energies 2013, 6, 5297–5313. [CrossRef] Yeow, T.S.; Cuerva, A.; Conan, B.; Pérez-Álvarez, J. Wind tunnel analysis of the detachment bubble on Bolund Island. J. Phys. Conf. Ser. 2014, 555, 012021. [CrossRef] Yeow, T.S.; Cuerva-Tejero, A.; Pérez-Álvarez, J. Reproducing the Bolund experiment in wind tunnel. Wind Energy 2015, 18, 153–169. [CrossRef] Chaudhari, A.; Hellsten, A.; Hämäläinen, J. Full-Scale Experimental Validation of Large-Eddy Simulation of Wind Flows over Complex Terrain: The Bolund Hill. Adv. Meteorol. 2016. [CrossRef] Conan, B.; Chaudhari, A.; Aubrun, S.; van Beeck, J.; Hämäläinen, J.; Hellsten, A. Experimental and numerical modelling of flow over complex terrain: The Bolund hill. Bound.-Layer Meteorol. 2016, 158, 183–208. [CrossRef]

Energies 2018, 11, 1694

11. 12. 13. 14. 15.

16. 17. 18. 19. 20.

21. 22.

23. 24. 25. 26.

14 of 14

Sessarego, M.; Shen, W.Z.; van der Laan, M.P.; Hansen, K.S.; Zhu, W.J. CFD Simulations of Flows in a Wind Farm in Complex Terrain and Comparisons to Measurements. Appl. Sci. 2018, 8, 788. [CrossRef] Astolfi, D.; Castellani, F.; Terzi, L. A Study of Wind Turbine Wakes in Complex Terrain through RANS Simulation and SCADA Data. J. Sol. Energy Eng. 2018, 140, 031001. [CrossRef] Uchida, T. LES Investigation of Terrain-Induced Turbulence in Complex Terrain and Economic Effects of Wind Turbine Control. Energies 2018, 11, 1530. [CrossRef] Uchida, T. Computational Fluid Dynamics (CFD) Investigation of Wind Turbine Nacelle Separation Accident over Complex Terrain in Japan. Energies 2018, 11, 1485. [CrossRef] Uchida, T.; Ohya, Y. Latest Developments in Numerical Wind Synopsis Prediction Using the RIAMCOMPACT CFD Model-Design Wind Speed Evaluation and Wind Risk (Terrain-Induced Turbulence) Diagnostics in Japan. Energies 2011, 4, 458–474. [CrossRef] Uchida, T. Large-Eddy Simulation and Wind Tunnel Experiment of Airflow over Bolund Hill. Open J. Fluid Dyn. 2018, 8, 30–43. [CrossRef] Uchida, T. High-Resolution LES of Terrain-Induced Turbulence around Wind Turbine Generators by Using Turbulent Inflow Boundary Conditions. Open J. Fluid Dyn. 2017, 7, 511–524. [CrossRef] Uchida, T. High-Resolution Micro-Siting Technique for Large Scale Wind Farm Outside of Japan Using LES Turbulence Model. Energy Power Eng. 2017, 9, 802–813. [CrossRef] Uchida, T. CFD Prediction of the Airflow at a Large-Scale Wind Farm above a Steep, Three-Dimensional Escarpment. Energy Power Eng. 2017, 9, 829–842. [CrossRef] Uchida, T.; Ohya, Y. Verification of the Prediction Accuracy of Annual Energy Output at Noma Wind Park by the Non-Stationary and Non-Linear Wind Synopsis Simulator, RIAM-COMPACT. J. Fluid Sci. Technol. 2008, 3, 344–358. [CrossRef] Uchida, T.; Ohya, Y. Micro-siting Technique for Wind Turbine Generators by Using Large-Eddy Simulation. J. Wind Eng. Ind. Aerodyn. 2008, 96, 2121–2138. [CrossRef] Uchida, T.; Maruyama, T.; Ohya, Y. New Evaluation Technique for WTG Design Wind Speed using a CFD-model-based Unsteady Flow Simulation with Wind Direction Changes. Model. Simul. Eng. 2011. [CrossRef] Kim, J.; Moin, P. Application of a fractional-step method to incompressible Navier-Stokes equations. J. Comput. Phys. 1985, 59, 308–323. [CrossRef] Kajishima, T. Upstream-shifted interpolation method for numerical simulation of incompressible flows. Bull. Jpn. Soc. Mech. Eng. B 1994, 60, 3319–3326. (In Japanese) [CrossRef] Kawamura, T.; Takami, H.; Kuwahara, K. Computation of high Reynolds number flow around a circular cylinder with surface roughness. Fluid Dyn. Res. 1986, 1, 145–162. [CrossRef] Smagorinsky, J. General circulation experiments with the primitive equations, Part 1, Basic experiments. Mon. Weather Rev. 1963, 91, 99–164. [CrossRef] © 2018 by the author. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).

Suggest Documents