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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 high speed aerodynamics, shock/boundary layer interaction, and various engineering aspects of detonation (which includes pulsed detonation engines). 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.
============ New for 2009 ============
Continued experimental testing of pulsed detonation engines with upgrades in ignition systems and fuel in a collaborative project with the National University of Singapore.
Preliminary continuous detonation wave engine studies in a collaborative project with HyPerComp, Inc. along with detonation engine cycle analysis.
Professor Frank K. Lu becomes an internet star with the release of his AIAA “When did you know?” video.
Computational research involving detonation physics. These studies represent a continuation of previous work aimed at developing an improved understanding of detonation for various engineering applications.
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. This is a collaborative effort with Dr. Chaoqun Liu of UT Arlington's Department of Mathematics. A recent article about this work can be found on the TACC website.
Continued improvements to the low-speed and supersonic wind tunnel facilities.
Small scale supersonic wind tunnel: construction. Continuation in small scale undegraduate lab facilities.