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MEM425F09.HW5.soln

MEM425F09.HW5.soln - solution Problem 6.4 Equation...

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MEM 425: Aircraft Performance & Design Home work #5 (due 10/29/09) Relevance to Program Outcomes a-k : a, e, k --------------------------------------------------------------------------------------------------------- 1. Problem 6.4 2. Problem 6.1 – use maximum lift coefficient of 1.3; consider both thrust- limit and stall-limit cases; assume load-limit is not a constraint.
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Unformatted text preview: solution Problem 6.4 Equation 6.16 (given) From this, Problem 6.1: 6.1: For a sustained turn, the minimum turn radius and maximum turn rate will be restricted by either the maximum thrust available, the stall velocity, or maximum allowable load factor....
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