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Tijdeman, H. (author), van Nunen, J.W.G. (author), Kraan, A.N. (author), Persoon, A.J. (author), Poestkoke, R. (author), Roos, R. (author), Schippers, P. (author), Siebert, C.M. (author)A wind-tunnel investigation was carried out on an oscillating model of the F-5 wing with and without an external store (AIM-9J missile). Detailed steady and unsteady pressure distributions were obtained over the wing, while on the store total aerodynamic loads were measured. The tests covered the Mach number range between Ma = 0.6 and Ma = 1.35,...report 1979
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Tijdeman, H. (author), van Nunen, J.W.G. (author), Kraan, A.N. (author), Persoon, A.J. (author), Poestkoke, R. (author), Roos, R. (author), Schippers, P. (author), Siebert, C.M. (author)A wind-tunnel investigation was carried out on an oscillating model of the F-5 wing with and without an external store (AIM-9J missile). Detailed steady and unsteady pressure distributions were obtained over the wing, while on the store total aerodynamic loads were measured. The tests covered the Mach number range between Ma = 0.6 and Ma = 1.35,...report 1979
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Tijdeman, H. (author), van Nunen, J.W.G. (author), Kraan, A.N. (author), Persoon, A.J. (author), Poestkoke, R. (author), Roos, R. (author), Schippers, P. (author), Siebert, C.M. (author)A wind-tunnel investigation was carried out on an oscillating ng model of the F-5 wing with and without an external store (AIM-9J missile) . Detailed steady and unsteady pressure distributions were obtained over the wing, while on the store total aerodynamic loads were obtained. In addition, wind-tunnel wall pressures were measured. The tests...report 1978