Drag and Stability Characteristics of a Variety of Reefed and Unreefed Parachute Configurations at Mach 1.80 with an Empirical Correlation for Supersonic Mach Numbers

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National Aeronautics and Space Administration, 1975 - Aerodynamics, Supersonic - 109 pages
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Contents

Section 1
28
Section 2
93
Section 3
96

2 other sections not shown

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