Numerical prediction of aerothermodynamic effects on a re-entry vehicle body flap configuration-Reference-Cited by-同舟云学术

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Numerical prediction of aerothermodynamic effects on a re-entry vehicle body flap configuration

Published:2009-07 Issue:1-2 Volume:65 Page:221-239
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Di Clemente Marco,Marini Marco,Di Benedetto Sara,Schettino Antonio,Ranuzzi Giuliano

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference17 articles.

1. A. Schettino, M. Marini, R. Donelli, PRO.R.A. USV enabling technologies in aerothermodynamics, Scope of Work, CIRA-CF-05-0116, April 2005.

2. A. Schettino, E. Bucchignani, Software and numerical design of H3NS, CIRA-TR-AEP-99-126, June 2000.

3. G. Ranuzzi, S. Borreca, H3NS: code development verification and validation, CIRA-CF-06-1017, September 2006.

4. M. Di Clemente, Requirements for PWT shock wave boundary layer interaction experiments, CIRA-CF-04-0693, December 2004.

5. J. Muylaert, et al., EXPERT system requirements document (ESRD), TOS-MPA/2745/JM Is. 2, Rev. 0, May 2003.

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