Analysis of Aeroheating Augmentation due to Reaction Control System Jets on Orion Crew Exploration Vehicle
暂无分享,去创建一个
[1] Paul M. Danehy,et al. Experimental Measurement of RCS Jet Interaction Effects on a Capsule Entry Vehicle , 2008 .
[2] Thomas J. Horvath,et al. Aeroheating Testing and Predictions for Project Orion CEV at Turbulent Conditions , 2008 .
[3] M. Pindzola,et al. JET SIMULATION IN GROUND TEST FACILITIES , 1963 .
[4] William I. Scallion,et al. Aerodynamic Challenges for the Mars Science Laboratory Entry, Descent and Landing , 2009 .
[5] Brian R. Hollis,et al. High-Enthalpy Aerothermodynamics of a Mars Entry Vehicle Part 2: Computational Results , 1997 .
[6] Von Doenhoff,et al. A preliminary investigation of boundary-layer transition along a flat plate with adverse pressure gradient , 1938 .
[7] L. A. Cassel,et al. Aerodynamic Interference Induced by Reaction Controls , 1973 .
[8] Thomas J. Horvath,et al. Experimental Hypersonic Aerodynamic Characteristics of Mars Surveyor 2001 Precision Lander with Flap , 2006 .
[9] J. J. Bertin,et al. Heat-transfer rate and pressure measurements obtained during Apollo orbital entries , 1970 .
[10] G. Candler,et al. Data-Parallel Line Relaxation Method for the Navier -Stokes Equations , 1998 .
[11] Dean R. Chapman,et al. Preliminary report on a study of separated flows in supersonic and subsonic streams , 1956 .