A Determination of the Laminar-, Transitional-, and Turbulent-boundary-layer Temperature-recovery Factors on a Flat Plate in Supersonic Flow
1950-06-01
Miscellaneous
No indication
English
BOUNDARY LAYER - TEMPERATURE , BOUNDARY LAYER - PLATES, FLAT EFFECT OF TEMPERATURE , WIND TUNNEL TESTS - AAL - HEAT TRANSFER, SUPERSONIC (6') , FLOW VELOCITY, HIGH - SUPERSONIC , BOUNDARY LAYER - VELOCITY DISTRIBUTION , BOUNDARY LAYER - PLATES, FLAT TURBULENT , WIND TUNNELS - AAL - HEAT TRANSFER, SUPERSONIC (6') (AMER ) , HEAT TRANSMISSION - BOUNDARY LAYER , BOUNDARY LAYER - PLATES, FLAT LAMINAR , BOUNDARY LAYER TRANSITION - PLATES, FLAT
Engineering Index Backfile | 1950
|Turbulent boundary-layer temperature recovery factors in two-dimensional supersonic flow
Engineering Index Backfile | 1951
|