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Flow Solver Predicts Condensation During Supersonic Wind Tunnel Tests Project Purpose: The goal of this project is to use High Performance Computers (HPCs) and Computational Fluid Dynamics (CFD) to test Scramjet aircraft
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Document Date: 2011-12-06 15:32:10
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File Size: 78,11 KB
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IndustryTerm
code developer /
/
Person
Jack Edwards /
Susan Cox-Stouffer /
/
/
Position
REACTMB-MP /
/
Product
Sapphire /
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Technology
Condensation /
Fluid Dynamics /
ten processors /
simulation /
/
SocialTag
Aerodynamics
Jet engines
Spacecraft propulsion
Aircraft engines
Scramjet
Computational fluid dynamics
Supersonic wind tunnel
Ramjet
Wind tunnel
Aerospace engineering