Comment on "A Re-Entry Control Effectiveness Methodology for the Space Shuttle Orbiter"
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[1] M. D. Bennett. Velocity of bodies powered by diatomic cold-gas thrusters , 1976 .
[2] J. P. Reding,et al. Reynolds number criticality in dynamic tests , 1978 .
[3] J. P. Reding,et al. Unsteady aerodynamic analysis of space shuttle vehicles. Part 4: Effect of control deflections on orbiter unsteady aerodynamics , 1973 .
[4] J. P. Reding,et al. Review of delta wing space shuttle vehicle dynamics , 1971 .
[5] John C. Adams,et al. Hypersonic Lifting Body Windward Surface Flow-Field Analysis for High Angles of Incidence , 1973 .
[6] Lars E. Ericsson,et al. Effects of Delta Wing Separation on Shuttle Dynamics , 1973 .
[7] H. L. Giles,et al. Analysis of hypersonic pressure and heat transfer tests on a flat plate with a flap and a delta wing with body, elevons, fins, and rudders Final report , 1966 .
[8] J. P. Reding,et al. Scaling problems in dynamic tests of aircraft-like configurations , 1978 .
[9] H. L. Seegmiller,et al. Surface flow patterns and aerodynamic heating on space shuttle vehicles , 1971 .
[10] H. Ikawa. A Re-entry Control Effectiveness Methodology for the Space Shuttle Orbiter , 1977 .
[11] M. D. Bennett. Velocity of Bodies Powered by Rapidly Discharged Cold-Gas Thrusters , 1975 .
[12] Rolf A. Guenther,et al. Nonexistence of axisymmetric separated flow. , 1969 .
[13] J. W. Keyes,et al. Flow phenomena and separation over delta wings with trailing-edge flaps at Mach 6. , 1968 .