Iterative PNS algorithms for solving 3-D supersonic flows with upstream influences-Reference-Cited by-同舟云学术

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Iterative PNS algorithms for solving 3-D supersonic flows with upstream influences

Published:2000-01-10 Issue: Volume: Page:
ISSN:
Container-title:38th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Tannehill John¹,Miller James²,Lawrence Scott³

Affiliation:

1. Iowa State Univ., Ames

2. Engineering Analysis, Inc., Ames, IA

3. NASA, Ames Research Center, Moffett Field, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-821

Reference25 articles.

1. PNS algorithm for solving supersonic flows with upstream influences

2. Application of the IPNS algorithm to complex two-dimensional body geometries

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1. Study of effect of a smooth hump on hypersonic boundary layer instability;Theoretical and Computational Fluid Dynamics;2016-05-27

2. Influence of two-dimensional smooth humps on linear and non-linear instability of a supersonic boundary layer;Computers & Fluids;2013-06

3. New Forward/Backward Sweeping Parabolized Navier-Stokes Algorithm;Journal of Spacecraft and Rockets;2003-03

4. Development of a forward-backward sweeping parabolized Navier-Stokes algorithm;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14

5. Computation of hypersonic laminar separated flows using an iterated PNS algorithm;39th Aerospace Sciences Meeting and Exhibit;2001-01-08

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