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 |
Checkout 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 |