Evaluation of boundary-layer and parabolized Navier-Stokes solutionsfor re-entry vehicles
- 1 January 1986
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 23 (1) , 70-78
- https://doi.org/10.2514/3.25085
Abstract
No abstract availableKeywords
This publication has 15 references indexed in Scilit:
- Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edgesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Inviscid Flowfield Calculations for Re-entry Vehicles with Control SurfacesAIAA Journal, 1977
- Three-dimensional supersonic flow of a viscous or inviscid gasJournal of Computational Physics, 1975
- Calculation of the Flow on a Cone at High Angle of AttackAIAA Journal, 1974
- Viscous flow over a cone at moderate incidence—IComputers & Fluids, 1973
- A calculation procedure for heat, mass and momentum transfer in three-dimensional parabolic flowsInternational Journal of Heat and Mass Transfer, 1972
- An alternating directional implicit scheme for three-dimensional hypersonic flowsJournal of Computational Physics, 1971
- Application of the unsteady numerical method of Godunov to computation of supersonic flows past bell-shaped bodiesJournal of Computational Physics, 1970
- Hypersonic interactions near sharp leading edges.AIAA Journal, 1969
- Hypersonic viscous drag effects on blunt slender conesAIAA Journal, 1964