Computation of nonequilibrium merged stagnation shock layers by successive accelerated replacement
- 16 June 1969
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Measured and predicted air ionization in blunt body shock layersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Merged stagnation shock layer of nonequilibrium dissociating gas.AIAA Journal, 1968
- Application of the method of nonlinear simultaneous displacements togeneral three- dimensional stagnation point boundary layer equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Method of accelerated successive replacement applied to boundary-layer equations.AIAA Journal, 1968
- Convective and radiative heat transfer during superorbital entry.AIAA Journal, 1967
- Viscous nonequilibrium blunt-body flow.AIAA Journal, 1967
- Machine calculation of compressible laminar boundary layersAIAA Journal, 1965
- Numerical solution of nonlinear two-point boundary problems by finite difference methodsCommunications of the ACM, 1964
- RAREFIED HYPERSONIC FLOW OVER A SPHEREPublished by Elsevier ,1962
- Viscous Aerodynamic Characteristics in Hypersonic Rarefied Gas FlowJournal of the Aerospace Sciences, 1960