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Static Aerodynamic Characteristics, Pressure Distributions, and RAM-air Inflation of Attached Inflatable Decelerator Models at Mach 3.0
William D. Deveikis
Jan 1970
· 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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Okuningi ngo-William D. Deveikis
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Local Aerodynamic Heat Transfer and Boundary-layer Transition on Roughened Sphere-ellipsoid Bodies at Mach Number 3.0
William D. Deveikis
Mahhala
Investigation of the Compressive Strength and Creep of 7075-T6 Aluminum-alloy Plates at Elevated Temperatures
William D. Deveikis
Mahhala
Flow Patterns and Pressure Distributions Around a Bluff Afterbody in the Wake of a 120° Cone for Various Separation Distances at Mach 3.0
William D. Deveikis
Mahhala
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
Mahhala
Ama-e-book afanayo
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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
Mahhala