Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges
- 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:
- Solution of the multidimensional compressible Navier-Stokes equations by a generalized implicit methodJournal of Computational Physics, 1977
- An implicit finite-difference algorithm for hyperbolic systems in conservation-law formJournal of Computational Physics, 1976
- Aerodynamic characteristics of slender wings with sharp leading edges - A reviewJournal of Aircraft, 1976
- Numerical Computation of Two-Dimensional Viscous Blunt Body Flows with an Impinging ShockAIAA Journal, 1976
- A numerical study of supersonic viscous cone flow at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Numerical Solution for Three-Dimensional Inviscid Supersonic FlowAIAA Journal, 1972
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971