Computation of Subsonic Inviscid Flow past a Cone Using High-Order Schemes-Reference-Cited by-同舟云学术

Computation of Subsonic Inviscid Flow past a Cone Using High-Order Schemes

Published:2002-10 Issue:10 Volume:40 Page:1961-1968
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Kim Jae Wook¹,Morris Philip J.¹

Affiliation:

1. Pennsylvania State University, University Park, Pennsylvania 16802

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1557

Reference10 articles.

1. Experiments on the low-speed flow past cones

2. Aerodynamic noise prediction using parallel methods on unstructured grids

3. Souliez, F. J. “Parallel Methods for Computing Unsteady Separated Flows Around Complex Geometries,” Ph.D. Dissertation, Dept. of Aerospace Engineering,PennsylvaniaState Univ.University Park, PA,Aug. 2002.

4. Optimized compact finite difference schemes with maximum resolution

5. Implementation of Boundary Conditions for Optimized High-Order Compact Schemes

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