![Aerodynamics / Wind tunnels / Langley Research Center / Supersonic wind tunnel / National Transonic Facility / Scramjet / Mach number / Unitary Plan Wind Tunnel / Eight-Foot High Speed Tunnel / Aerospace engineering / Fluid dynamics / Dynamics Aerodynamics / Wind tunnels / Langley Research Center / Supersonic wind tunnel / National Transonic Facility / Scramjet / Mach number / Unitary Plan Wind Tunnel / Eight-Foot High Speed Tunnel / Aerospace engineering / Fluid dynamics / Dynamics](https://www.pdfsearch.io/img/197ec8c6aa6b114013a136a40da91cf7.jpg)
| Document Date: 2013-06-26 22:07:44 Open Document File Size: 71,13 KBShare Result on Facebook
Company IBM / Lear / / Country United States / / Facility Transonic Dynamics Tunnel / Foot High Temperature Tunnel / Inch Supersonic Wind Tunnel / Foot Vertical Spin Tunnel Unitary Plan Wind Tunnel / Disturbance Tunnel / theNASA Langley Transonic Dynamics Tunnel / Foot Transonic Tunnel / Foot Subsonic Tunnel / NASA Langley’s Impact Dynamics Research Facility / Langley Wind Tunnels National Transonic Facility Transonic Dynamics Tunnel / Supersonic Low Disturbance Tunnel / CF4 Tunnel / Quiet Tunnel Basic Aerodynamics Research Tunnel / National Transonic Facility / Helium Tunnel / Foot High Temperature Tunnel Low Turbulence Pressure Tunnel / / IndustryTerm air transportation system / electronics research / space technology / / Organization National Aeronautics and Space Administration / / Position General / / Product F/A-18 / / ProvinceOrState Virginia / / Technology simulation / Animation / /
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