UNIIFIED %u21CNOSE-TO -TAIL%u21D COMPUTATIONAL METHOD FOR HYPERSONIC VEHICLE APPLICATIONS

Author:

CHAKRAVARTHY S.R.1,SZEMA K.Y.1,HANEY J.W.2

Affiliation:

1. ROCKWELL INTERNATIONAL SCIENCE CENTER, THOUSAND OAKS, CA

2. ROCKWELL INTERNATIONAL, LAKEWOOD, CA

Publisher

American Institute of Aeronautics and Astronautics

Reference24 articles.

1. tored Implicit UpwindSchemes," AIAAPaper 84-0165, 1984.

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1. Experimental and Computational Study of Underexpanded Jet Impingement Heat Transfer;41st AIAA Thermophysics Conference;2009-06-14

2. Advancements in Multidisciplinary Design Optimization Applied to Hypersonic Vehicles to Achieve Performance Closure;15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2008-04-28

3. Parametric Shape Study of Capsule-Type Vehicles During Atmospheric Re-entry;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2006-06-25

4. CFD simulations in support of Shuttle Orbiter contingency abort aerodynamic database enhancement;35th AIAA Thermophysics Conference;2001-06-11

5. Conversion of a single process CFD code to distributed and massively parallel processing;Advances in Engineering Software;1998-04

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