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EAS4101_S11_HW7Q

# EAS4101_S11_HW7Q - b Dv C as a function of c The lift slope...

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EAS 4101 - Aerodynamics – Spring 2011 1/1 HW#3 2/23/11, 7 th Homework 1. Problem 1: Given: A thin, symmetric, untwisted rectangular wing of AR = 6 flying at a geometric angle of attack α possessing a chord c . Find: Evaluate the fundamental equation of Prandtl’s lifting line theory at the following 4 stations along the wing: θ = π / 8, π / 4, 3 π / 8, and π / 2. a) L C as a function of . b)
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Unformatted text preview: b) Dv C as a function of . c) The lift slope, a. 2. Problem 7.1 from Bertin’s “Aerodynamics for Engineers” 3. Problem 7.2 from Bertin’s “Aerodynamics for Engineers” 4. Problem 7.3 from Bertin’s “Aerodynamics for Engineers” 5. Problem 7.4 from Bertin’s “Aerodynamics for Engineers” 6. Problem 7.5 from Bertin’s “Aerodynamics for Engineers”...
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