Static Aerodynamic Characteristics, Pressure Distributions, and RAM-air Inflation of Attached Inflatable Decelerator Models at Mach 3.0

· National Aeronautics and Space Administration
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Static aerodynamic characteristics, pressure distributions, and ram air inflation of attached inflatable drag chute models at supersonic speed.

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同類型電子書

Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack: Subsonic, Transonic, and Supersonic Speeds, Issues 1301-1310
A. Gerald Rainey
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