Wind tunnel wall interference corrections for aircraft models in the transonic regime
暂无分享,去创建一个
[1] S. Davis,et al. Adaptive-wall wind-tunnel development for transonic testing , 1981 .
[2] M. H. Rizk. Propeller slipstream/wing interaction in the transonic regime , 1981 .
[3] E. Murman. A CORRECTION METHOD FOR TRANSONIC WIND TUNNEL WALL INTERFERENCE , 1979 .
[4] W. R. Sears,et al. Self correcting wind tunnels , 1973, The Aeronautical Journal (1968).
[5] A. Ferri,et al. A method for transonic wind-tunnel corrections. , 1973 .
[6] Robert G. Joppa,et al. Development of Minimum-Correction Wind Tunnels , 1976 .
[7] W. Sickles,et al. Application of adaptive-wall techniques in a three-dimensional wind tunnel with variable wall porosity , 1980 .
[8] H. C. Garner,et al. SUBSONIC WIND TUNNEL WALL CORRECTIONS , 1966 .
[9] Magdi H. Rizk,et al. The Single-Cycle Scheme: A New Approach to Numerical Optimization , 1983 .
[10] Wind-tunnel wall interference corrections for three-dimensional flows , 1982 .
[11] W. B. Kemp. Toward the correctable-interference transonic wind tunnel , 1976 .
[12] M. Rizk. A new approach to optimization for aerodynamic applications , 1983 .
[13] William B. Kemp. A Slotted Test Section Numerical Model for Interference Assessment , 1985 .
[14] H. Keller,et al. Analysis of Numerical Methods , 1969 .
[15] J C Erickson,et al. Adaptive-Wall Wind-Tunnel Investigations , 1981 .
[16] L. Ohman,et al. Application of the fast Fourier transform to two-dimensional wind tunnel wall interference , 1980 .