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 |