MEM425F09.HW5

MEM425F09.HW5 - 1. Problem 6.4 2. Problem 6.1 – use...

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Peter Carrion MEM 425 10/29/2009 MEM 425: Aircraft Performance & Design Home work #5 (due 10/29/09) Relevance to Program Outcomes a-k : a, e, k ------------------------------------------------------------------------------------------------------
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Unformatted text preview: 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. Peter Carrion MEM 425 10/29/2009...
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This note was uploaded on 12/06/2009 for the course MEM 425 taught by Professor Yousuff during the Fall '08 term at Drexel.

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MEM425F09.HW5 - 1. Problem 6.4 2. Problem 6.1 – use...

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