Spin Tunnel Investigation of a 1/30 Scale Model of the North American A-5A Airplane
Description:
"An investigation has been made in the Langley spin tunnel to determine the erect and inverted spin and recovery characteristics of a 1/30-scale dynamic model of the North American A-5A airplane. Tests were made for the basic flight design loading with the center of gravity at 30-percent mean aerodynamic chord and also for a forward position and a rearward position with the center of gravity at 26-percent and 40-percent mean aerodynamic chord, respectively. Tests were also made to determine the…
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Date:
June 1964
Creator:
Lee, Henry A.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department