Hypersonics and Hypervelocity Research

UDRI Hypersonic Wind Tunnel Model

Designing, Analyzing, Developing, and Testing for Efficiency and Safety at Hypersonic Speeds

UDRI's hypersonic and hypervelocity research supports our customers' efforts to better understand and mitigate the thermal and aerodynamic stresses involved in hypersonic flight (over five times the speed of sound). We work to make hypersonic flight a safer and more efficient reality.

Top: UDRI-designed hypersonic vehicle wind tunnel model tested in the Air Force Research Laboratory’s Mach 6 High Reynolds Facility at Wright-Patterson AFB.

Hypersonic Flow

UDRI performs Computational Fluid Dynamics (CFD) modeling of hypersonic flows to better guide the design process and limit cases that may not be safe or cost effective.

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Hypersonic Test Apparatus

UDRI researchers design, fabricate, and commission complex hypersonic test apparatus, including the Mach 6 Ludwieg Tube wind tunnel for the Air Force Research Laboratory.

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Hypervelocity Impact Testing

UDRI performs hypervelocity impact testing on materials and structures for NASA systems to see how they will endure impact from space dust and debris traveling at hypersonic speeds.

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Vehicle Structures

UDRI researchers design, analyze, develop, and test hypersonic materials, components, and systems for commercial and military customers.

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CONTACT

University of Dayton Research Institute


300 College Park
Dayton, Ohio 45469 - 7759
937-229-2113
Email