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Unformatted text preview: fuselage. 2. Now for the general case, not the specific 787 values in problem #1, solve for the percentage change in induced drag created by a 1% reduction in aircraft weight. Assume that the wing remains unchanged. Begin with a sentence, then an equation, then another sentence, and so on, alternating explanations and equations until you are completed....
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This note was uploaded on 02/21/2012 for the course AAE 334 taught by Professor Collicott during the Fall '09 term at Purdue UniversityWest Lafayette.
 Fall '09
 COLLICOTT

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