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Incipient- and developed-spin and recovery characteristics of a modern high-speed fighter design with low aspect ratio as determined from dynamic-model tests /

Title:Incipient- and developed-spin and recovery characteristics of a modern high-speed fighter design with low aspect ratio as determined from dynamic-model tests /
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Note:Washington, [D.C.] : National Aeronautics and Space Administration, 1961
  
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Subject:Dynamic models
Subject:Aircraft stability
Subject:Aerodynamic coefficients
Subject:Yawing moments
Subject:Pitching moments
Subject:Stability derivatives
Subject:Windtunnel tests
Subject:Aircraft design
Subject:Low aspect ratio
Subject:Fighter aircraft
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