Wind-tunnel investigation of the aerodynamic and structural deflection characteristics of the Goodyear inflatoplane /
by Bennie W. Cocke, Jr.

Description

Main Author: Cocke, Bennie W., Jr.
Related Names: United States. National Advisory Committee for Aeronautics.
Langley Aeronautical Laboratory.
Language(s): English
Published: Washington, D.C. : NACA, 1958.
Subjects: Aerodynamics > Aerodynamics / Research.
Research aircraft.
Summary: Summary: An investigation has been conducted in the Langley full-scale tunnel to determine the aerodynamic and structural deflection characteristics of the Goodyear Inflatoplane over a range of test velocities from minimum stall speed up to speeds giving load factors for wing buckling. Tests were conducted over a range of speeds from approximately 41 to 70 mph with wing-guy-cable loads, wing-distortion photographs, and aerodynamic-force data recorded at each speed for a full range of angle of attack.
Note: "Report date September 10, 1958."
Also available in electronic format.
Physical Description: 56 p. : ill. ; 28 cm.
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