Numerical solution of the hypersonic viscous shock-layer equations
- 1 May 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (5) , 843-851
- https://doi.org/10.2514/3.5776
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Surface conditions on hyperboloids and paraboloids in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- VISCOUS, HYPERSONIC FLOW AROUND A BLUNT BODYPublished by Defense Technical Information Center (DTIC) ,1968
- Near wake uniqueness and a re-examination of the throat concept in laminar mixing theoryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Laminar flow past a sphere at high Mach numberJournal of Fluid Mechanics, 1966
- Second-order boundary-layer effects in hypersonic flow past axisymmetric blunt bodiesJournal of Fluid Mechanics, 1964
- On the viscous hypersonic blunt body problemJournal of Fluid Mechanics, 1964
- On Heat Transfer in Slip FlowJournal of the Aerospace Sciences, 1958