THEORETICAL INVESTIGATIONS OF A SUPERSONIC LAMINAR BOUNDARY LAYER WITH FOREIGN-GAS INJECTION
- 1 January 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (1) , 148-158
- https://doi.org/10.2514/3.1484
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A review of binary laminar boundary layer characteristicsInternational Journal of Heat and Mass Transfer, 1961
- MEASUREMENT OF RECOVERY FACTORS AND HEAT TRANSFER COEFFICIENTS WITH TRANSPIRATION COOLING IN A TURBULENT BOUNDARY LAYER AT M=3 USING AIR AND HELIUM AS COOLANTSPublished by Defense Technical Information Center (DTIC) ,1956