Calculation of axisymmetric inlet flowfield using the Euler equations
- 13 July 1983
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Transonic wing-body calculations using Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- A multiple grid scheme for solving the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Transonic Inlet Flow Calculations Using a General Grid-Generation SchemeJournal of Fluids Engineering, 1980
- Transonic potential flow computation about three-dimensional inlets,ducts and bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Calculation of Transonic Inlet Flowfields Using Generalized CoordinatesJournal of Aircraft, 1980
- Accelerated Iterative Calculation of Transonic Nacelle FlowfieldsAIAA Journal, 1977
- Transonic Potential Flow around Axisymmetric Inlets and Bodies at Angle of AttackAIAA Journal, 1977
- Cartesian Mesh Solution for Axisymmetric Transonic Potential Flow Around InletsAIAA Journal, 1977
- Calculation of Transonic Flow around Axisymmetric InletsAIAA Journal, 1975