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Dynamics / Fluid mechanics / Aerodynamics / Spacecraft propulsion / Unstart / Turbine / Pressure coefficient / Turbojet / Hypersonic speed / Jet engines / Aerospace engineering / Fluid dynamics


Mach 4 Test Results of a Dual-Flowpath, Turbine Based Combined Cycle Inlet Cindy W. Albertson,1 Saied Emami,2 and Carl A. Trexler3
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Document Date: 2013-04-10 16:43:41


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File Size: 524,63 KB

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Company

Pratt & Whitney / Facility National Aero / /

Facility

B. Test Facility / Hampton University / American Institute of Aeronautics / Blow Down Facility / /

IndustryTerm

lower flow energy loss / flowmeter/back pressure device / backpressure device / low energy boundary layer / flowmeter/back pressuring device / /

NaturalFeature

TBCC inlet / /

Organization

National Aeronautics and Space Administration / American Institute of Aeronautics and Astronautics Subscripts / Hampton University / American Institute of Aeronautics / /

Person

Cindy W. Albertson / Hypersonic Airbreathing / /

Position

Senior Research Engineer / Research Engineer / /

ProgrammingLanguage

Labview / /

ProvinceOrState

Virginia / /

RadioStation

H FM / /

SocialTag