Publication Date:
2016-06-07
Description:
Aeronautical design engineering for general aviation aircraft considers the iteration of wind tunnel test data are lift, weight, drag, and thrust as the basic balancing factor in drag reduction efforts.
Keywords:
AIRCRAFT DESIGN, TESTING AND PERFORMANCE
Type:
Kansas Univ. Proc. of the NASA, Ind., Univ., Gen. Aviation Drag Reduction Workshop; p 77-85
Format:
application/pdf
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