Floating Shock Fitting for Cones at Large Incidence
- 1 April 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 16 (4) , 385-392
- https://doi.org/10.2514/3.60900
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Computation of three-dimensional, inviscid supersonic flowsPublished by Springer Nature ,2008
- Some results of calculations of flows around conical bodies at large incidence anglesPublished by Springer Nature ,2008
- A numerical study of supersonic viscous cone flow at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Vortical singularity behind a highly yawed coneAIAA Journal, 1975
- On the shape of the shock in nonsymmetric hypersonic flow around a circular coneFluid Dynamics, 1975
- Supersonic flow past circular cones at large angles of attackFluid Dynamics, 1975
- Calculation of the supersonic flow around conical bodiesUSSR Computational Mathematics and Mathematical Physics, 1973
- Numerical Solution for Three-Dimensional Inviscid Supersonic FlowAIAA Journal, 1972
- The effect of viscosity in hypervelocity impact crateringPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Vortical singularities in conical flow.AIAA Journal, 1967