Overview of Experimental Investigations for Ares I Launch Vehicle Development
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-13
Reference5 articles.
1. 1Hall, R. M., Holland, S. D., and Blevins, J.A. "Aerodynamic Characterization of a Modern Launch Vehicle," AIAA AerospaceSciencesMeeting,NASACP10817,2011.
2. 2Erickson, G. E., and Wilcox, F. J. "Ares I Aerodynamic Testing at the NASA Langley Unitary Plan Wind Tunnel," AIAA AerospaceSciencesMeeting, NASACP10544,2011.
3. 3Pinier, J. T., Niskey, C. J., Hanke, J. L., and Tomek, W. G. "Ares I Aerodynamic Testing at the Boeing Polysonic Wind Tunnel,"AIAAAerospaceSciencesMeeting,NASACP10848,2011.
4. 4Capone, F. J., Paulson, J., and Erickson, G. E. "Lift-off and Transition Aerodynamics of the Ares I (A106) Launch Vehicle,"AIAAAerospaceSciencesMeeting,NASACP10649,2011.
5. 5Pinier, J. T., and Niskey, C. J. "Ares I and Ares I-X Stage Separation Aerodynamic Testing," AIAA Aerospace Sciences Meeting,NASACP10840,2011.
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1. Detailed Uncertainty Analysis of the Ares I A106 Liftoff/Transition Database;Journal of Spacecraft and Rockets;2012-09
2. Assessment of Computational-Fluid-Dynamics-Based Response Surface Database for Ares I Supersonic Ascent Aerodynamics;Journal of Spacecraft and Rockets;2012-07
3. Detailed Uncertainty Analysis of the Ares I A106 Liftoff/Transition Database;29th AIAA Applied Aerodynamics Conference;2011-06-27
4. Assessment of CFD-based Response Surface Model for Ares I Supersonic Ascent Aerodynamics;29th AIAA Applied Aerodynamics Conference;2011-06-27
5. The Crucial Role of Error Correlation for Uncertainty Modeling of CFD-Based Aerodynamics Increments;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
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