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Lambert's W Function in Maple Robert M. Corless, 1 Gaston H. Gonnet, 2 D. E. G. Hare, 3 and David J. Jerey 4
De nition and Notation
Many users of Maple have encountered a function called W . The simplest way one might meet this function is shown in the following session fragment. >solve(w*exp(w)=x,w);
W(x)
What is this function, and why is it in Maple? The rst part of that question is already answered by the above Maple session: W (x) is de ned to be `the' solution to the equation wew = x. Actually, for some values of x, this equation has more than one root, in which case the dierent solutions are called branches of W . The way we handle branches is described later. The reason why W is included in Maple is simply that it has appeared in the solution of enough problems to have earned the right to have a name of its own. [For a function, getting your own name is rather like Pinocchio getting to be a real boy.] This article concentrates on the real-valued branches of W and their manipulation in Maple. It is problem-oriented, because we found that the investigation of Lambert's W function was very pleasant, and believe that some of that pleasure is best transmitted by a participatory article | that is, one that leaves some work for the reader. Readers are encouraged to try the problems at the end of the article, using Maple as required. A more detailed paper [4] is available which discusses the complex-valued function W (z ) and its Maple implementation. A PostScript version of [4] can be obtained by anonymous ftp to cs-archive.uwaterloo.ca, from the directory cs-archive/CS-93-03, and also by anonymous ftp to the Maple share library, from the le maple/5.2/doc/LambertW.ps. Notation: The letter W is now a standard notation for this function, following early Maple usage. In [4] we proposed to call this Lambert's W function, because Lambert set the rst problem which required W for its solution, and because Euler attributed the series with which he solved the problem to Lambert. In [3], it is also called the `omega' function, because there is a persistent rumor that there are papers which use the greek letter ! for this function. If any readers of this article can provide a reference for this notation, please inform us by e-mail to [email protected]. If x is real, then for ?1=e x < 0 there are two possible real values of W (x) (see Figure 1). We denote the branch satisfying ?1 W (x) by W (x), and the branch satisfying W (x) ?1 by W (x). W (x) is referred to as the principal branch of the W function. This notation is dierent from that used in [4], which agrees with the intended notation for the research version of Maple, whereas the notation of the present article agrees with the implemented notation for 0
Dept. Applied Math, University of Western Ontario, London, Canada, [email protected] Dept. Informatik, ETH, Zurich, Switzerland, [email protected] 3 Symbolic Computation Group, University of Waterloo, Waterloo, Canada, [email protected] 4 Dept. Applied Math, University of Western Ontario, London, Canada, [email protected]
1
2
12
Lambert's W function Maple V Release 2. Finally, we sometimes get sloppy and use W to indicate both real branches, or either branch, or even sometimes a complex branch, whenever this is clear from the context.
W 1 −1/e
x
−1
1
2
3
−1 −2 −3 −4
Figure 1. The two real branches of W (x). ||, W (x); { { {, W (x). 0
Sample Applications
Members of the maple_group electronic mailing list may recall some discussions of the W function. The following problems have been taken from those discussions, plus some other sources. Solution of a Jet Fuel Problem
This problem was contributed to maple_group by Michael Kamprath, with commentary by Harald Hanche-Olsen. Consider the following equations, which describe the endurance Et and range R of a jet airplane. We wish to nd the thrust speci c fuel consumption ct and the weight of the fuel w ? w , given the physical constants describing the plane and its environment. The equations are [1] (p. 312) 0
1
Et = cCCL log ww t D 2CL = = 2 w ?w = ; R = c C S 0
1
1 2
t D
1 2
1 2
0
1
where Et is the endurance, CL and CD are the lift and drag coecients, w is the initial weight of the plane, w is the nal weight of the plane, R is the range, S is the planform area of the 0
1
13
Lambert's W function plane's wings, and is the ambient air density. We simplify these equations by rst grouping the physical parameters and nondimensionalizing. We put w = w =w and c = Et CD ct =CL , and introduce the new parameter p = A = ? 2Et w : 1
R
0
0
1 2
SCL
The equations then become c = ? log(w) and pw 1 ? 2A log(w) = 1 : This equation has exactly one real solution if A < 0, since the left-hand side is a strictly increasing function of W . It can be solved in terms of W , the solution being