Numerical calculations of the transient loading of blunt obstacles by shocks in air.
- 1 March 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (3) , 460-467
- https://doi.org/10.2514/3.3459
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Numerical calculation of supersonic wake flow.AIAA Journal, 1965
- A direct method for computation of nonequilibrium flows with detached shock wavesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- Computing Transient Gas Flows with Shock WavesPhysics of Fluids, 1964
- Shock and Hot Spot Initiation of Homogeneous ExplosivesPhysics of Fluids, 1963