A direct method for calculation of the flow about an axisymmetric blunt body at angle of attack.
Open Access
- 1 May 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (5) , 776-782
- https://doi.org/10.2514/3.3546
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- A direct method for computation of nonequilibrium flows with detached shock waves.AIAA Journal, 1966
- Hypersonic blunt-body flow fields at angle of attackAIAA Journal, 1964
- Transonic rotational flow over a convex cornerJournal of Fluid Mechanics, 1960
- Weak solutions of nonlinear hyperbolic equations and their numerical computationCommunications on Pure and Applied Mathematics, 1954