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Aerodynamics / Jet engines / Spacecraft propulsion / Aircraft engines / Scramjet / Computational fluid dynamics / Supersonic wind tunnel / Ramjet / Wind tunnel / Aerospace engineering / Fluid mechanics / Fluid dynamics


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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code developer / /

Person

Jack Edwards / Susan Cox-Stouffer / /

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Position

REACTMB-MP / /

Product

Sapphire / /

Technology

Condensation / Fluid Dynamics / ten processors / simulation / /

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