Unformatted text preview: 3. Roughly estimate the maximum coefficients of Lift and Drag based on the data available for these aircraft. Also estimate the wing loading (weight-to-wingarea W/S ratio) and the thrust-to-weight T/W ratio. This is an open ended home work. The accuracy of the numbers is not important, but you need to explain clearly how you determined them. Include reference to the source for your information....
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- Fall '08
- Aerodynamics, Fixed-wing aircraft, Wing, Lift, Program Outcomes a-k