Implicit Algorithm for the Conservative Transonic Full-Potential Equation Using an Arbitrary Mesh
- 1 October 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 17 (10) , 1038-1045
- https://doi.org/10.2514/3.61274
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Numerical solution for airfoils near stall in optimized boundary-fitted curvilinear coordinatesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Implicit approximate-factorization schemes for the efficient solution of steady transonic flow problemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Automatic numerical generation of body-fitted curvilinear coordinate system for field containing any number of arbitrary two-dimensional bodiesJournal of Computational Physics, 1974
- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974
- Conservation equations of gasdynamics in curvilinear coordinate systemsJournal of Computational Physics, 1974
- ANALYSIS OF EMBEDDED SHOCK WAVES CALCULATED BY RELAXATION METHODSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Alternating direction methods for parabolic equations in two space dimensions with a mixed derivativeThe Computer Journal, 1970
- Plane subcritical flow past a lifting aerofoilProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1969
- A detached shock calculation by second-order finite differencesJournal of Computational Physics, 1967
- Weak solutions of nonlinear hyperbolic equations and their numerical computationCommunications on Pure and Applied Mathematics, 1954