Measurement of Experimental Boundary Conditions for CFD Validation of a Supersonic Jet in Transonic Crossflow-Reference-Cited by-同舟云学术

Measurement of Experimental Boundary Conditions for CFD Validation of a Supersonic Jet in Transonic Crossflow

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Beresh Steven¹,Henfling John¹,Spillers Russell¹,Erven Rocky¹

Affiliation:

1. Sandia National Laboratories

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3449

Reference25 articles.

1. Perspective on computational fluid dynamics validation

2. 2American Institute of Aeronautics and Astronautics, "Guide for the Verification and Validation of Computational Fluid Dynamics Simulations,"AIAA G-077-1998,1998.

3. Experimental Methodology for Computational Fluid Dynamics Code Validation

4. Issues in Computational Fluid Dynamics Code Verification and Validation

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