Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition / John W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009.

Author/creator Slater, John W.
Other author Saunders, John D.
Other author NASA Glenn Research Center.
Other author AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference 2009 : Bremen, Germany)
Format Electronic
Publication InfoCleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Description1 online resource (27 p.) : ill.
Supplemental Contenthttps://purl.fdlp.gov/GPO/gpo4610

SeriesNASA/TM ; 2010-216362
NASA technical memorandum 216362. ^A467613
General noteTitle from title screen (viewed on March 3, 2011).
General note"May 2010."
General note"AIAA-2009-7349."
General noteGPO Cataloging Record Distribution Program (CRDP).
Bibliography noteIncludes bibliographical references (p. 27)
Funding informationWBS 138494.04.01.01
GPO item number0830-D (online)
Govt. docs number NAS 1.15:2010-216362

Availability

Library Location Call Number Status Item Actions
Electronic Resources Access Content Online ✔ Available