Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows
By: A.R. Porro ... [et al.].
Contributors: Porro, A. R.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Series: NASA technical paper -- 3142.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; For sale by the National Technical Information Service]
Published: 1991
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 26
Subjects: Aerodynamics, Hypersonic.; Aerodynamics, Supersonic.; Boundary layer.; Boundary layers.; Compressible flow.; Honeycomb structures.; Hypersonic flow.; Supersonic flow.; Turbulent boundary layer.; Wind tunnel models.
Notes: "August 1991"--Cover.

Includes bibliographical references (p. 26).

Also available via Internet from the NTRS web site. Address as of 3/16/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910018822%5F1991018822.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1991. 1 microfiche : negative.