Navier-Stokes computations of a prolate spheroid at angle of attack
- 1 November 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 26 (11), 986-993
- https://doi.org/10.2514/3.45871
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Navier-Stokes computations of prolate spheroids at angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Accurate numerical solutions for transonic viscous flow over finite wingsJournal of Aircraft, 1987
- Comparison of finite volume flux vector splittings for the Euler equationsAIAA Journal, 1986
- Far-field boundary conditions for transonic lifting solutions to theEuler equationsAIAA Journal, 1986
- Characteristic-Based Schemes for the Euler EquationsAnnual Review of Fluid Mechanics, 1986
- Boundary layers and separation on a spheroid at incidenceAIAA Journal, 1985
- Computation of supersonic viscous flows around pointed bodies at large incidencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- A method for the calculation of three-dimensional boundary layers with circumferential reversed flow on bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982