Welcome to the UT Arlington Aerodynamics Research Center webpage. The Aerodynamics Research Center has existed at the university in one form or another since the 1930's when it was originally an aircraft maintenance and fabrication facility. In 1986, the present building was constructed that allowed for a large expansion of equipment, which now includes lowspeed, transonic, supersonic, and hypersonic facilities. Current research has focused on classical and high speed aerodynamics, various aspects of detonation (which includes pulsed detonation engines), shock interaction and electromagnetic flow control. In addition to the experimental facilities, we have extensive capabilities to study and test aerodynamic models using Computational Fluid Dynamics (CFD). The experimental test results can be used to validate the CFD models, and vice-versa. Our clients include corporate and government entities as can be seen on our sponsors page. |
| ============News for 2008 ============ |
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Welcome to Dr. Luca Massa, who joined the ARC faculty group in August. His areas of expertise are in combustion, detonation, rocket motors, flow stability, CFD and high performance parallel computing |
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Continued experimental testing of pulsed detonation engines with upgrades in ignition systems and fuel. |
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Electromagnetic boundary layer flow control using artificially seeded air flow to raise conductivity. Experiments will be carried out in the low-speed and supersonic wind tunnels. |
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Detonation: experimental and computational. This represents a continuation of previous work aimed at developing an improved understanding of detonation for applications. |
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Passive control of shock/boundary-layer interactions using micro vortex generators. The experimental studies will be carried out in the supersonic wind tunnel and used to validate a high order DNS/LES computational flow model. Collaborative effort with Dr. Chaoqun Liu of UT Arlington's Department of Mathematics. |
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Continued improvements to the low-speed and supersonic wind tunnel facilities. |
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Small scale supersonic wind tunnel: construction. Continuation in small scale undegraduate facilities. |