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Modeling of Shock Tunnel Aeroheating Data on the Mars Science Laboratory Aeroshell

Wright, Michael J. and Olejniczak, Joe and Brown, James L. and Hornung, Hans G. and Edquist, Karl T. (2006) Modeling of Shock Tunnel Aeroheating Data on the Mars Science Laboratory Aeroshell. Journal of Thermophysics and Heat Transfer, 20 (4). pp. 641-651. ISSN 0887-8722.

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Additional Information:This material is declared a work of the U.S. Government and is not subject to copyright protection in the United States. Presented as Paper 0177 at the 43rd Aerospace Sciences Meeting and Exhibit, Reno, NV, 10–13 January 2005; received 5 September 2005; revision received 13 November 2005; accepted for publication 16 November 2005. Support for this work was provided to NASA Ames and Langley Research Centers by the Mars Technology Program in support of the Mars Science Laboratory mission. The California Institute of Technology was funded by the Jet Propulsion Laboratory under contract No. JPL PO #1256067. The authors would like to thank Jeff Umland (Jet Propulsion Laboratory) for his support, as well as Dan Reda (Ames) and Brian Hollis (Langley) for discussions on turbulent transition criteria in flight and ground test facilities.
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Jet Propulsion LaboratoryJPL PO #1256067
Issue or Number:4
Record Number:CaltechAUTHORS:WRIjtht06
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Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:11299
Deposited By: Archive Administrator
Deposited On:29 Jul 2008 22:31
Last Modified:03 Oct 2019 00:17

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