Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at supersonic speeds
By: Hyun D. Kim, Franco C. Frate.
Contributors: Frate, Franco C.; NASA Glenn Research Center.
Series: [NASA technical memorandum] -- NASA/TM-2001-210565; NASA technical memorandum -- 201565.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for Aerospace Information
Published: 2001
Place of publication: [Cleveland, Ohio]; Hanover, MD
Language: eng
Format: Microform
Subjects: Aerodynamic characteristics.; Angle of attack.; Computational fluid dynamics.; Dimensional analysis.; Boundary layer transition.; Flow distribution.
Notes: Shipping list no.: 2003-0099-M.

Also available via Internet from the NASA web site. Address as of 2/24/03: http://gltrs.grc.nasa.gov/reports/2001/TM-2001-210565.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?] 1 microfiche.