Validation of a Computer Code for Analysis of Subsonic Aerodynamic Performance of Wings with Flaps in Combination with a Canard Or Horizontal Tail and an Application to Optimization

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National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990 - Airplanes - 122 pages
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Contents

Section 1
28
Section 2
35
Section 3
116

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