Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration

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Название: Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration

Автор:

Издательство: NASA

Страниц: 123

Формат: PDF

Размер: 22 Мб

Качество: Хорошее

Год: 1993

Язык: английский

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A supersonic wind tunnel investigation was conducted in the NASA Langley Unitary Plan Wind Tunnel on an advanced derivative configuration of the United States Air Force F-16 fighter. Longitudinal and lateral directional force and moment data were obtained at Mach numbers of 1.60 to 2.16 to evaluate basic performance parameters and control effectiveness. The aerodynamic characteristics for the F-16 derivative model were compared with the data obtained for the F-16C model and also with a previously tested generic wing model that features an identical plan form shape and similar twist distribution.

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