Investigation of the aerodynamic characteristics of a hypersonic transport model at Mach numbers to 6
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[1] R. H. Petersen,et al. Performance tradeoffs and research problems for hypersonic transports , 1965 .
[2] W. Sears. On projectiles of minimum wave drag , 1947 .
[3] R. M. Hicks,et al. Use of grit-type boundary-layer transition trips on wind-tunnel models , 1966 .
[4] D. B. Spalding,et al. The drag of a compressible turbulent boundary layer on a smooth flat plate with and without heat transfer , 1964, Journal of Fluid Mechanics.
[5] E. Polhamus. A concept of the vortex lift of sharp-edge delta wings based on a leading-edge-suction analogy , 1966 .
[6] J. W. Keyes,et al. Flow phenomena and separation over delta wings with trailing-edge flaps at Mach 6. , 1968 .
[7] William T. Schaefer,et al. Characteristics of Major Active Wind Tunnels at the Langley Research Center , 1965 .
[8] F. S. Kirkham,et al. Aerodynamic characteristics of a hypersonic transport configuration at Mach 6.86 , 1970 .
[9] Arvel E. Gentry,et al. Hypersonic Arbitrary-Body Aerodynamic Computer Program MARK III Version. Volume 2. Program Formulation and Listings , 1968 .
[10] J. A. Penland,et al. Comparative aerodynamic study of two hypersonic cruise aircraft configurations derived from trade-off studies , 1967 .
[11] R. J. Margason,et al. Vortex-lattice FORTRAN program for estimating subsonic aerodynamic characteristics of complex planforms , 1971 .