A pseudo-unsteady approach for predicting steady supersonic flows
Author:
Affiliation:
1. Texas, University, Arlington
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-541
Reference27 articles.
1. Hypersonic viscous flow over slender bodies with sharp leading edges.
2. Calculation of the Flow on a Cone at High Angle of Attack
3. Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges
4. A Review of Marching Procedures for Parabolized Navier-Stokes Equations
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1. Parabolized Navier-Stokes Algorithm for Solving Supersonic Flows with Upstream Influences;AIAA Journal;2000-10
2. Iterative PNS algorithms for solving 3-D supersonic flows with upstream influences;38th Aerospace Sciences Meeting and Exhibit;2000-01-10
3. Development of an iterative PNS code for separated flows;14th Computational Fluid Dynamics Conference;1999-08-22
4. PNS algorithm for solving supersonic flows with upstream influences;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12
5. Computation of supersonic flows with embedded separated regions using an efficient PNS algorithm;13th Computational Fluid Dynamics Conference;1997-06-29
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