An efficient, full-potential implicit method based on characteristics for supersonic flows
- 1 September 1983
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 21 (9) , 1262-1270
- https://doi.org/10.2514/3.8238
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Computation of three-dimensional, inviscid supersonic flowsPublished by Springer Nature ,2008
- Conservative Full Potential, Implicit Marching Scheme for Supersonic FlowsAIAA Journal, 1982
- Computation of nonlinear supersonic potential flow over three dimensional surfacesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Fast, Conservative Algorithm for Solving the Transonic Full-Potential EquationAIAA Journal, 1980
- Investigation of Crossflow Shocks on Delta Wings in Supersonic FlowAIAA Journal, 1980
- Automatic mesh-point clustering near a boundary in grid generation with elliptic partial differential equationsJournal of Computational Physics, 1979
- Numerical Procedure for the Computation of Irrotational Conical FlowsAIAA Journal, 1979
- Weak solutions of nonlinear hyperbolic equations and their numerical computationCommunications on Pure and Applied Mathematics, 1954