Transonic airfoil calculations using solution-adaptive grids
- 22 June 1981
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Fast, Conservative Algorithm for Solving the Transonic Full-Potential EquationAIAA Journal, 1980
- Generation of Body-Fitted Coordinates Using Hyperbolic Partial Differential EquationsSIAM Journal on Scientific and Statistical Computing, 1980
- Adaptive Grid Method for Problems in Fluid Mechanics and Heat TransferAIAA Journal, 1980
- Optimal Nodal Point Distribution for Improved Accuracy in Computational Fluid DynamicsAIAA Journal, 1980
- Automatic mesh-point clustering near a boundary in grid generation with elliptic partial differential equationsJournal of Computational Physics, 1979
- Implicit Algorithm for the Conservative Transonic Full-Potential Equation Using an Arbitrary MeshAIAA Journal, 1979
- Numerical solutions for viscous and potential flow about arbitrary two-dimensional bodies using body-fitted coordinate systemsJournal of Computational Physics, 1977
- Automatic numerical generation of body-fitted curvilinear coordinate system for field containing any number of arbitrary two-dimensional bodiesJournal of Computational Physics, 1974
- Conservation equations of gasdynamics in curvilinear coordinate systemsJournal of Computational Physics, 1974
- A detached shock calculation by second-order finite differencesJournal of Computational Physics, 1967