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Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds

Donald Isaacs

1966

Páginas: 39

Género: Ailerons

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Theoretical study of the rolling response of aircraft to turbulent air

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Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap

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Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance

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