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