Mass transfer and first-order boundary-layer effects on sharp cone drag. II - At hypersonic conditions.
- 1 November 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (11) , 1954-1960
- https://doi.org/10.2514/3.3824
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Hypersonic viscous drag effects on blunt slender conesAIAA Journal, 1964
- Effect of mass injection on the drag of a slender cone in hypersonic flowAIAA Journal, 1964
- Laminar heat transfer to spherically blunted cones at hypersonic conditionsAIAA Journal, 1964
- SOLUTION OF THE GENERAL BOUNDARY-LAYER EQUATIONS FOR COMPRESSIBLE LAMINAR FLOW, INCLUDING TRANSVERSE CURVATUREPublished by Defense Technical Information Center (DTIC) ,1963
- HYPERSONIC FLOW OVER A SLENDER CONE WITH GAS INJECTIONPublished by Defense Technical Information Center (DTIC) ,1962