Question
For a finite wing with an elliptical planform, using the given circulation distribution along the span and Prandtl's Lifting Line Theory, derive the following properties
For a finite wing with an elliptical planform, using the given circulation distribution along the span and Prandtl's Lifting Line Theory, derive the following properties and point out the important findings:
a) Downwash velocity distribution along the span. (25 pts)
b) Lift distribution along the span. (25 pts)
c) Induced angle of attack distribution along the span. (25 pts)
d) Induced drag coefficient distribution along the span. (25 pts)
Elliptical circulation distribution:
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Fundamentals Of Hydraulic Engineering Systems
Authors: Robert J. Houghtalen, A. Osman H. Akan, Ned H. C. Hwang
4th Edition
136016383, 978-0136016380
