Computational fluid dynamics nose-to-tail capability - Hypersonic unsteady Navier-Stokes code validation
- 1 March 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 27 (2) , 123-130
- https://doi.org/10.2514/3.26116
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Simulation of transonic viscous flow over a fighter-like configuration including inletJournal of Aircraft, 1989
- Advances in the computation of transonic separated flows over finite wingsComputers & Fluids, 1989
- Transonic wing flows using an Euler/Navier-Stokes zonal approachJournal of Aircraft, 1987
- Numerical simulation of unsteady, viscous, high-angle-of-attack flows using a partially flux-split algorithmPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Real-gas flowfields about three-dimensional configurationsJournal of Spacecraft and Rockets, 1985
- An implicit finite-difference algorithm for hyperbolic systems in conservation-law formJournal of Computational Physics, 1976
- CHEMICALLY REACTING VISCOUS FLOW PROGRAM FOR MULTI-COMPONENT GAS MIXTURES.Published by Office of Scientific and Technical Information (OSTI) ,1971