Finite difference solution of the laminar boundary layer equations including second-order effects
- 24 June 1968
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- MASS TRANSFER AND FIRST-ORDER BOUNDARY -LAYER EFFECTS ON SHARP CONE DRAGPublished by Defense Technical Information Center (DTIC) ,1966
- Mass transfer and first-order boundary-layer effects on sharp cone dragPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966
- Effect of mass injection on the drag of a slender cone in hypersonic flowAIAA Journal, 1964
- A STUDY OF FINITE-DIFFERENCE METHODS AS APPLIED TO HYPERSONIC VISCOUS SHOCK-LAYER EQUATIONSPublished by Defense Technical Information Center (DTIC) ,1963
- HYPERSONIC FLOW OVER A SLENDER CONE WITH GAS INJECTIONPublished by Defense Technical Information Center (DTIC) ,1962
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949