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....
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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.
- Fall '08