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Dynamics / Jet engines / Airspeed / Spacecraft propulsion / Rocket-based combined cycle / Hypersonic speed / Supersonic wind tunnel / Wind tunnel / Mach number / Aerospace engineering / Aerodynamics / Fluid dynamics


1- by 1-Foot Supersonic Wind Tunnel at NASA Glenn Research Center
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Document Date: 2011-11-07 08:48:34

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File Size: 692,56 KB

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Facility

Facility Testing / NASA’s Glenn Research Center / Facility Benefits / Foot Supersonic Wind Tunnel / Facility Description The / /

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IndustryTerm

probe actuation systems / accessible real-time data display / oil flow visualization / /

NaturalFeature

GTX inlet / /

Organization

NASA’s Glenn Research Center in Cleveland / Ohio PS / National Aeronautics and Space Administration / /

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Position

Facility Manager / /

Product

GTX / /

ProvinceOrState

Ohio / /

Technology

Fluid Dynamics / /

URL

www.nasa.gov / http /

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