NASA Technical Reports Server (NTRS) : Results pdf

NASA Technical Reports Server (NTRS) : Results

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Description of the Book:

A 0.03-scale model of the 747 CAM/Orbiter was tested in an 8 x 12 foot transonic wind tunnel. Dynamic loads, pressure, and empennage flow field data were obtained using pressure transducers, strain gages, and a split film anemometer. The test variables included Mach number, angle of attack, sideslip angle, orbiter tailcone on and off, orbiter partial tailcone, orbiter nozzle air scoops, orbiter body flap angle, and orbiter elevon angle

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 10/1/1976
• Year: 1976
• Book Topics/Themes: NASA Technical Reports Server (NTRS), DYNAMIC LOADS, DYNAMIC PRESSURE, SPACE SHUTTLE ORBITERS, SUPERSONIC AIRCRAFT, TRANSONIC WIND TUNNELS, ANGLE OF ATTACK, FLOW DISTRIBUTION, MACH NUMBER, PRESSURE SENSORS, SUBSONIC SPEED, WIND TUNNEL TESTS

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