Aer E 261 Project

Aer E 261 Project - Aer E 261 Project#2 Find TR for given...

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Aer E 261 Project #2 10/03/2008 20:25:00 Find TR for given altitude and Mach # AKA – DRAG Cd = CD,0 + K(CL^2) o CD,0 = 0.02326 for M < 0.8 o CD,0 = 1.6484M^2 – 2.6374M + 1.0785
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Unformatted text preview: • TR = (1/2)rho*V^2*S*(Cd) • AR = b^2/S • K = 0.049261 • 10/03/2008 20:25:00 ← 10/03/2008 20:25:00 ←...
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