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

Bibliographic Details

Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Program
Other Authors:	Porro, A. R. (A. Robert)
Format:	Government Document Microform Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; 1991.
Series:	NASA technical paper ; 3142.
Subjects:	Aerodynamics, Hypersonic. Aerodynamics, Supersonic. Boundary layer. Boundary layers. Compressible flow. Honeycomb structures. Hypersonic flow. Supersonic flow. Turbulent boundary layer. Wind tunnel models.
Online Access:	https://purl.fdlp.gov/GPO/LPS67809