Supersonic Retropropulsion Dynamic Data Analysis from NASA Langley Unitary Plan Wind Tunnel
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[1] J. W. Keyes,et al. Effect of forward-facing jets on aerodynamic characteristics of blunt configurations at Mach 6. , 1967 .
[2] P. O. Jarvinen,et al. The aerodynamic characteristics of large angled cones with retrorockets , 1970 .
[3] E. Naudascher,et al. Self-Sustained Oscillations of Impinging Free Shear Layers , 1979 .
[4] Thomas Janoski,et al. Introduction to Time-Series Analysis , 1994 .
[5] R. Manning,et al. Mars Exploration Entry, Descent, and Landing Challenges , 2007 .
[6] Robert D. Braun,et al. High Mass Mars Entry, Descent, and Landing Architecture Assessment , 2009 .
[7] David J. Kinney,et al. Entry, Descent and Landing Systems Analysis Study: Phase 1 Report , 2010 .
[8] Ravi Prakash,et al. Development of Supersonic Retro-Propulsion for Future Mars Entry, Descent, and Landing Systems , 2010 .
[9] Kerry Trumble. An Initial Assessment of Navier-Stokes Codes Applied to Supersonic Retro-Propulsion , 2010 .
[10] Robert D. Braun,et al. Performance Characterization of Supersonic Retropropulsion for High-Mass Mars Entry Systems , 2010 .
[11] Scott A. Berry,et al. Analysis of Dynamic Data from Supersonic Retropropulsion Experiments in NASA Langley's Unitary Plan Wind Tunnel , 2012 .
[12] Matthew N. Rhode,et al. Estimation of Uncertainties for a Supersonic Retro- Propulsion Model Validation Experiment in a Wind Tunnel , 2012 .
[13] D. G. Schauerhamer,et al. Supersonic retropropulsion CFD validation with Ames Unitary Plan Wind Tunnel test data , 2013, 2013 IEEE Aerospace Conference.
[14] Karl T. Edquist,et al. Analysis of Navier–Stokes Codes Applied to Supersonic Retropropulsion Wind-Tunnel Test , 2014 .
[15] Scott A. Berry,et al. Supersonic Retropropulsion Experimental Results from NASA Ames 9×7 Foot Supersonic Wind Tunnel , 2014 .
[16] Scott A. Berry,et al. Supersonic Retropropulsion Validation Experiment in the NASA Langley Unitary Plan Wind Tunnel , 2014 .
[17] Karl T. Edquist,et al. Supersonic Retropropulsion Computational Fluid Dynamics Validation with Langley 4×4 Foot Test Data , 2014 .
[18] Karl T. Edquist,et al. Development of Supersonic Retropropulsion for Future Mars Entry, Descent, and Landing Systems , 2014 .