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Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration have a 60©� delta wing and a high unwept horizontal tail

Control hinge-movement and effectiveness characteristics of several interchangeable tip controls on a 60©� delta wing at Mach numbers of 1.41, 1.62, and 1.96

Calculated effects of the lateral acceleration derivatives on the dynamic lateral stability of a delta-wing airplane

Published Year

• 1950-1959 (3) *

Subject

• Delta wing airplanes (3) *
• Airplanes--Wings, Triangular (1)
• Stability of airplanes, Lateral--Mathematical models (1)
• Stability of airplanes, Longitudinal (1)

Author

• Campbell, John P. (1)
• Mitchell, Jesse L. (1)
• Morris, Odell A. (1)
• Peck, Robert F. (1)
• Woodling, Carroll H. (1)

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