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Fluid dynamics / Turbine / Computational fluid dynamics / Hypersonic speed / Overflow / Axial compressor / Vortex / Turbomachinery / Wind tunnel / Aerodynamics / Aerospace engineering / Fluid mechanics


20 HIGH-END COMPUTING AT NASA 2007–2008 AERONAUTICS RESEARCH MISSION DIRECTORATE
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Document Date: 2009-08-07 18:35:18

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File Size: 3,01 MB

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City

Seattle / San Antonio / Miami / /

Company

Honeywell Engine Co. / AVETEC Inc. / Reno NV / ANSYS / General Electric Company / /

Country

United States / Columbia / /

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Event

FDA Phase / /

Facility

NASA Glenn Research Center / NAS facility / University of Toledo / /

IndustryTerm

simulation tools / aeromechanics computational tool / later post-processing / parallel processing / flow simulation tools / flow control devices / vehicle systems / computational tools / air transportation system / actuator technologies / offshore oil platform access / thermal protection systems / gas turbine engine subsystems / multidisciplinary solutions / improved physics-based computational tools / crucial services / fidelity computational tools / possible flow control devices / gas turbine engine / rotor-blade trim algorithm / /

NaturalFeature

Integrated Inlet / Force-sponsored Versatile Active Highly Integrated Inlet / Lockheed inlet / /

Organization

Old Dominion University / NASA Glenn Research Center / NASA’s Aeronautics Research Mission Directorate / University of Toledo / US Federal Reserve / National Aeronautics and Space Administration / Aeronautics Research Mission Directorate / Army Vehicle Technology Directorate / Air Force / MISSION DIRECTORATE Ponnampalam Balakumar NASA Langley Research Center / /

Person

Chung Chang / Wai Ming / Kursat Kara / Terry Holst / Ethan Romander / Jasim Ahmad / Michael Hathaway / Jeff Dalton / David Kao / Osama A. Kandil / Ambady Suresh / Reynolds-Averaged Navier-Stokes / Thomas Pulliam / Neal M. Chaderjian / JAIWON SHIN / /

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Position

Rotor Grid Assistant / Administrator / /

Product

Toledo / H3D / /

ProvinceOrState

Texas / /

Technology

24 processors / fluid dynamics / 64 processors / 291 processors / actuator technologies / rotor-blade trim algorithm / flow control / aero / simulation / animation / parallel processing / /

URL

http /

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