Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows /

Saved in:
Bibliographic Details
Imprint:[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1991.
Description:26 pages : illustrations ; 28 cm.
Language:English
Series:NASA technical paper ; 3142
NASA technical paper ; 3142.
Subject:Aerodynamics, Hypersonic.
Aerodynamics, Supersonic.
Boundary layer.
Boundary layers.
Compressible flow.
Honeycomb structures.
Hypersonic flow.
Supersonic flow.
Turbulent boundary layer.
Wind tunnel models.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6505388
Hidden Bibliographic Details
Other authors / contributors:Porro, A. Robert.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Notes:"August 1991"--Cover.
Includes bibliographical references (page 26).
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.
GPO item no.:0830-H-15 (MF)
0830-H-15 (online)
Govt.docs classification:NAS 1.60:3142