Aerodynamic Design and Performance of a Bent-Axis Geometry Vehicle
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[1] D. W. Kuntz,et al. A comparison of predicted and measured aeroheating on a reentry vehicle flap geometry , 1987 .
[2] G. F. Polansky,et al. Inviscid/boundary layer prediction of aeroheating on a bent-axis biconic , 1986 .
[3] Mitchell Thomas,et al. Atmospheric Flight of a Variable-Bend Body , 1979 .
[4] R. Noack,et al. Inviscid flow field analysis of maneuvering hypersonic vehicles using the SCM formulation and parabolic grid generation , 1985 .
[5] D. Anderson,et al. A Split-Coefficient/Locally Monotonic Scheme for Multishocked Supersonic Flow , 1982 .
[6] W. L. Oberkampf,et al. Evaluation of inviscid/boundary layer and parabolized Navier-Stokes solutions for design of reentry vehicles , 1984 .
[7] G. F. Polansky,et al. Inviscid/boundary layer prediction of aerodynamics for a bent-axis biconic geometry , 1986 .
[8] W. L. Oberkampf,et al. Evaluation of boundary-layer and parabolized Navier-Stokes solutionsfor re-entry vehicles , 1986 .