An implicit algorithm for the conservative transonic full potential equation using an arbitrary mesh
- 10 July 1978
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 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
- Supercritical Wing Sections IIPublished by Springer Nature ,1975
- 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
- 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