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Fluid mechanics / Wind tunnels / Airspeed / Langley Research Center / National Transonic Facility / Mach number / NASA X-43 / Hypersonic speed / National Advisory Committee for Aeronautics / Aerodynamics / Aerospace engineering / Fluid dynamics


Fact Sheet National Aeronautics and Space Administration Langley Research Center Hampton, Virginia[removed]
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Document Date: 2013-06-26 22:07:44


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File Size: 3,15 MB

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Company

Langley Memorial Aeronautical Laboratory / /

Country

United States / /

Event

Force Majeure / /

Facility

Foot Vertical Spin Tunnel / Foot Transonic Tunnel / National Transonic Facility The National Transonic Facility / Langley Memorial Aeronautical Laboratory / Low-Turbulence Pressure Tunnel The Langley Low-Turbulence Pressure Tunnel / Unitary Plan Wind Tunnel The Langley Unitary Plan Wind Tunnel / Foot High Temperature Tunnel / Jet Exit Test Facility Transonic Dynamics Tunnel The Langley Jet Exit Test Facility / Meter Transonic Cryogenic Tunnel / Low-Turbulence Pressure Tunnel / Foot Subsonic Tunnel / Langley Transonic Dynamics Tunnel / National Transonic Facility / Government / /

IndustryTerm

shadowgraph systems / data acquisition software / spinrecovery parachutes systems / gas leaks / minimal energy consumption / ultraviolet oil / Temperature sensitive paint / hypersonic propulsion systems / appropriate systems / test gas / fail-safe systems / paint / power systems / energy / /

Organization

National Advisory Committee for Aeronautics / U.S. Government / National Aeronautics and Space Administration / NASA Langley Research Center / /

Person

Osborne Reynolds / /

Position

model at specific locations / researcher / Major / /

Product

F-15 / F-18 / Shuttle / F-14 / B-1 / /

ProvinceOrState

Virginia / /

Technology

laser / fluid dynamics / heat transfer / simulation / /

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