Mach 10 experimental database of a three-dimensional scramjet inlet flow field
By: Scott D. Holland.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 4648.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from the National Technical Information Service
Published: 1995
Place of publication: Hampton, Va; [Springfield, VA
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Engine inlets.; Flow distribution.; Hypersonic speed.; Inlet flow.; Internal flow.; Laminar boundary layer.; Oblique shock waves.; Pressure measurement.; Shock wave interaction.; Supersonic combustion ramjet engines.; Three dimensional flow.; Wind tunnel tests.
Notes: Shipping List #: 96-0637-M.

Also available via Internet from the NASA web site. Address as of 6/21/05: http://techreports.larc.nasa.gov/ltrs/PDF/NASA-95-tm4648.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995]. 3 microfiches.