Boundary Layer Feature Extraction White Paper

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Background & Real Flow Visualization. Traditional Visualization of CFD results. Boundary Layer Characterization. Boundary Layer Characteristic Extraction.
Extraction of Boundary Layer Characteristics from Fluent Results Fluent 2005 CFD Summit, Dearborn, MI Kent P. Misegades, CEI Inc., Apex, NC

… analyze, visualize, communicate

Topics Background & Real Flow Visualization Traditional Visualization of CFD results Boundary Layer Characterization Boundary Layer Characteristic Extraction Other Techniques Future Work … analyze, visualize, communicate

Background Subject: Viscous, High-Speed, Compressible Flows Slender bodies & wings at low angle-of-attack High Reynolds numbers, thus thin boundary layers Shock / boundary layer interaction significant BL thickness and flow distortion in engine inlets Extensive laminar flow may exist, thus BL transition critical … analyze, visualize, communicate

Background

Boeing 787

Lockheed-Martin HCV

Aerion SSBJ

SAI SSBJ

Advanced Aircraft with Extensive Laminar Flow … analyze, visualize, communicate

Background High-Fidelity Fluent CFD Aerodynamic Simulations Accuracy now comparable to legacy lab aero codes Dense meshes needed for turbulence models & shocks Boundary layers for RANS+SA models are well resolved DNS, LES, DES all produce far more detail than RANS Traditional post-processing ignores rich data in results We need to return to basics & real flow visualization … analyze, visualize, communicate

Real Flow Visualization

Laminar BL Separation and Turbulent BL Reattachment, M. Selig, UIUC … analyze, visualize, communicate

Real Flow Visualization

Boundary Layer Surface Flow using Paint Dots, Flometrics … analyze, visualize, communicate

Real Flow Visualization

Schlieren Photographs, NASA … analyze, visualize, communicate

Real Flow Visualization

Shadowgraph of Spacecraft Model, NASA … analyze, visualize, communicate

CFD Visualization Fluent Test Case Geometry: ONERA M6 Wing Mesh: 884,736 hexahedra Reynolds Number: 11.34 million Freestream Mach Number: 0.84 Angle of Attack: 3.07 degrees M>1

Fluent 6.2 results courtesy Thomas Scheidegger, Fluent Inc. All images created using EnSight 8.0 from CEI, Inc. … analyze, visualize, communicate

CFD Visualization Simple Techniques Results displayed on model surfaces & clip planes • Velocity, Cp, density, Mach number, etc.

Derived variables • total pressure, vorticity, entropy, helicity, etc.

Velocity profiles • qualitatively depicts BL profiles, thickness, separation, etc.

Isosurfaces • total pressure, sonic (Mach=1), vorticity, entropy, etc. … analyze, visualize, communicate

CFD Visualization

Surface Pressure

Total Pressure on Clip Plane

Pressure on Clip Plane

Mach Number on Clip Plane … analyze, visualize, communicate

CFD Visualization Sophisticated Techniques Regions of Reverse flow • Streamwise velocity at a small offset distance from a surface

Surface-Restricted Traces • Oil flow analog, particle traces in laminar sublayer

Lines of BL Separation and Attachment • Singularities on surface

Shock surfaces & Dilitation Contours Schlieren & Shadowgraph simulation … analyze, visualize, communicate

CFD Visualization Reverse Flow

Offset Velocity Magnitude

Surface-Restricted Traces

Offset Vx

Surface Traces and Offset Velocity … analyze, visualize, communicate

CFD Visualization Shock Surface Extraction

Lines of BL Separation (green) Lines of BL Attachment (magenta)

… analyze, visualize, communicate

CFD Visualization

Velocity Profiles under BL Separation Bubble … analyze, visualize, communicate

CFD Visualization

Schlieren Simulation (|∇ ∇· |)

Shadowgraph Simulation (∇ ∇2 ) … analyze, visualize, communicate

BL Characterization

Boundary Layers on an Airfoil, NASA … analyze, visualize, communicate

BL Characterization Classical Boundary Layer Characteristics See: Abbott & von Doenhoff, Theory of Wing Sections Thickness (δ δ): distance at which u = 0.99 x U Displacement thickness (δ δ*): how BL displaces flow Momentum Thickness (Θ Θ): loss of momentum in BL Shape Factor (H = δ* / Θ): Θ) separation tendency Skin Friction Coefficient (Cf): viscous drag, transition … analyze, visualize, communicate

BL Characterization BL “Health” Indicator: Total Pressure Loss • Total pressure drops due to viscosity and shocks • Isosurface of 95% freestream Ptotal indicates BL growth • Distance from surface to this 95% isosurface is desired

Boundary Layer Transition • Of increasing importance for DNS, LES, DES results • Involves anaysis of variables at BL edge … analyze, visualize, communicate

BL Characteristic Extraction Incorporated in EnSight 8.x from CEI Classical BL Characteristics • Thickness, δ, determined by proprietary edge-finding algorithm developed at CEI • δ* and Θ are 1-D integrals computed on surface nodes • Shape Factor is simply H = δ* / Θ • Cf is computed on surface • Numerically intensive computations for irregular grids • All characteristics available as surface variables … analyze, visualize, communicate

BL Characteristic Extraction

BL Thickness, δ

BL Momentum Thickness, Θ

BL Displacement Thickness, δ*

Shape Factor, H … analyze, visualize, communicate

Other Techniques Elevated surfaces of BL characteristics “Distance to value” variable on surfaces Variables on edge of boundary layers BL transition indicators Animations of all techniques for transient flows … analyze, visualize, communicate

Other Techniques

Elevated Surface of δ

Elevated Surface of δ

Contour of 95% Ptotal

Distance to 95% Ptotal … analyze, visualize, communicate

Other Techniques

BL Thickness, δ

Distance to 95% Ptotal

… analyze, visualize, communicate

Future Work Further Validation against DPW-I & II DLR models Flow separation detection & reporting Laminar/turbulent area ratios Drag breakdown Interactive velocity profiling Smart flow mapping with GPS-like decluttering Faster methods, better defaults & filters … analyze, visualize, communicate

DPW-I DLR-F4

Pressure … analyze, visualize, communicate

DPW-I DLR-F4

Boundary Layer Thickness … analyze, visualize, communicate

DPW-I DLR-F4

Distance to 95% Ptotal … analyze, visualize, communicate

Thank You

Boeing 787

Boeing Commercial Airplane Company, for supporting this work Fluent Inc., for use of FLUENT and providing example datasets … analyze, visualize, communicate