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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

Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8

Published Year

• 1950-1959 (2)

Subject

• Stability of airplanes, Longitudinal (2) *
• Delta wing airplanes (1)

Author

• Peck, Robert F. (2) *
• Mitchell, Jesse L. (1)

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