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Fluid mechanics / Dynamics / Airspeed / Dimensionless numbers / Hypersonic speed / Pressure coefficient / Mach number / Drag / Schlieren / Aerodynamics / Fluid dynamics / Aerospace engineering


Document Date: 2001-01-04 15:35:57

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City

Washington / D.C. / NACA / Hampton / Washington / /

Company

Reno NV / General Dynamics / Astronautics Inc. / USAF Wright Laboratory / Wright Laboratory / Aerospace / /

Country

United States / /

Currency

ESP / /

Facility

VA Anthony M. Mitchell Ellis J. Boudreaux USAF Wright Laboratory Eglin Air Force Base / NASA Langley Research Center / Hypersonic Missiles Lawrence D. Huebner NASA Langley Research Center / Eglin AFB / The dome / Dome Flow Separation Shock Collar Test Facility The / American Institute of Aeronautics / /

IndustryTerm

paint / oil / steel / /

Organization

American Institute of Aeronautics and Astronautics / American Institute of Aeronautics / National Aeronautics and Space Administration / FOR HYPERSONIC MISSILES Lawrence D. Huebner* NASA Langley Research Center / /

Person

Anthony M. Mitchell / Ellis J. Boudreaux / Hypersonic Airbreathing / Lawrence D. Huebner / /

/

Position

Research Engineer / forward / Engineer / /

Product

C-4 / /

ProgrammingLanguage

FL / /

ProvinceOrState

Virginia / Florida / D.C. / /

Technology

fluid dynamics / heat transfer / /

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