Transonic wing-body calculations using Euler equations
- 10 January 1983
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- A nearly conformal grid-generation method for transonic wing-body flowfield calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Transfinite mesh generation and damped Euler equation algorithm for transonic flow around wing-body configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methodsJournal of Computational Physics, 1981
- Grid generation and transonic flow calculations for three-dimensional configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- The Split Coefficient Matrix method for hyperbolic systems of gasdynamic equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Approximation von Punktmengen durch implizite FunktionenZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1978
- Automatic numerical generation of body-fitted curvilinear coordinate system for field containing any number of arbitrary two-dimensional bodiesJournal of Computational Physics, 1974