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

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Published 1991 by National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, For sale by the National Technical Information Service] in [Washington, D.C.], [Springfield, Va .
Written in English

Subjects:

• Aerodynamics, Hypersonic.,
• Aerodynamics, Supersonic.,
• Boundary layer.,
• Boundary layers.,
• Compressible flow.,
• Honeycomb structures.,
• Hypersonic flow.,
• Supersonic flow.,
• Turbulent boundary layer.,
• Wind tunnel models.

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Edition Notes

Statement	A.R. Porro ... [et al.].
Series	NASA technical paper -- 3142.
Contributions	Porro, A. R., United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
The Physical Object
Format	Microform
Pagination	26 p.
Number of Pages	26
ID Numbers
Open Library	OL17726039M

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