Estimation of Uncertainties for a Supersonic Retro-Propulsion Model Validation Experiment in a Wind Tunnel
Author:
Affiliation:
1. NASA Langley Research Center
2. W. L. Oberkampf Consulting
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2707
Reference28 articles.
1. Edquist, K. T., Dyakonov, A. A., Korzun, A. M., Shidner, J. D., Studak, J. W., Tigges, M. A., Kipp, D. M., Prakash, R., Trumble, K. A., and Dupzyk, I. C. "Development of Supersonic Retro-Propulsion for Future Mars Entry, Decent, and Landing Systems," AIAA Paper 2010-5046,June2010.
2. Schauerhamer, D. G, Trumble, K. A., Kleb, W. L, Carlson, J-R., and Edquist, K. T. "Continuing Validation of ComputationalFluid Dynamics forSupersonicRetropropulsion,"AIAA Paper 2012-0864,January 2012.
3. Survey of Supersonic Retropropulsion Technology for Mars Entry, Descent, and Landing
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