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Военная историяSupersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration

Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration
Название: Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration
Автор: Fox, Mike C.; Forrest, Dana K
Издательство: NASA
Страниц: 123
Формат: PDF
Размер: 22 Мб
Качество: Хорошее
Год: 1993
Язык: английский
Для сайта: eKnigi.org

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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