Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows
Subtitle: progress report for the period ended December 31, 1989
By: by D. J. Singh and S. N. Tiwari ; prepared for National Aeronautics and Space Administration, Langley Research Center.
Contributors: Tiwari, S. N.; Old Dominion University. Research Foundation.; Langley Research Center.
Series: NASA CR -- 186451.; NASA contractor report -- NASA CR-186451.
Publisher: Old Dominion University Research Foundation; National Technical Information Service, distributor
Published: 1990
Place of publication: Norfolk, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamics, Hypersonic.; Viscous flow.; Navier-Stokes equations.; Blunt leading edges.; Flow distribution.; Forebodies.; Hypersonic flow.; National Aerospace Plane program.; Noses (Forebodies); Viscous flow.
Notes: Also available via Internet from the NASA Technical Report Server web site. Address as of 8/25/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011634%5F1990011634.pdf  ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 2 microfiches.