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Main Title Method for Predicting Compressible Turbulent Boundary Layers in Adverse Pressure Gradients.
Author Pinckne, S. Z. ;
CORP Author National Aeronautics and Space Administration. Langley Research Center, Langley Station, Va.
Year Published 1971
Report Number NASA-TM-X-2302 ;L-6802; 764-75-01-01;
Stock Number N71-32210
Additional Subjects Air breathing engines ; Compressible flow ; Hypersonic speed ; Pressure gradients ; Turbulent boundary layer ; Boundary layer transition ;
Holdings
Library Call Number Additional Info Location Last
Modified
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Status
NTIS  N71-32210 Some EPA libraries have a fiche copy filed under the call number shown. 07/26/2022
Collation 59p
Title Annotations +++Method for Predicting Compressible Turbulent Boundary Layers in Adverse Pressure Gradients Applied to Hypersonic Air Breathing Propulsion
PUB Date Free Form Aug 71,
Category Codes 20D; 80F
NTIS Prices PC A04 MF A01
Document Type NT
Cataloging Source NTIS/MT
Control Number 326505704
Origin NTIS
Type CAT