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Dynamics / Pitot tube / Boundary layer / Boundary-layer thickness / Reynolds number / Turbulence / Flow separation / Flow measurement / Shock wave / Fluid mechanics / Aerodynamics / Fluid dynamics


No. 68·129 EXPERIMENTS IN SUPERSONIC TURBULENT FLOW WITH LARGE DISTRIBUTED SURFACE INJECTION by
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Document Date: 2012-12-26 07:47:38

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City

Reading / NEW YORK / /

Company

Pcou co / Graduate Aeronautical Laboratories / TRW / Rand Corp. / /

Continent

Americas / /

Currency

USD / GBP / /

Facility

Institute of Technology Pasadena / Cambridge University / American Institute of Aeronaulics / E. E. ZUKOSKI California Institute of Technology Pasadena / Supersonic Wind Tunnel / California Institute of Technology / /

IndustryTerm

stainless-steel particles / foreign gas injection / stainless-steel tubing / self-similar solutions / self-similar solution / e -; / /

Organization

California Institute of Technology / Cambridge University / Institute of Technology Pasadena / Department of Aeronautics / Advanced Research Projects Agency / U. S. Army Research Office / Engineering Department / Aeronautics Department / American Institute of Aeronaulics and Astronautics / F. L. FERNAND.EZ and E. E. ZUKOSKI California Institute of Technology Pasadena / /

Person

Spencer / Daniel Guggenheim Jet Prop / Mugalev / V / /

Position

D. J. / author and / Professor of Engineering / V. P. / /

Product

No. 68·129 EXPERIMENTS IN SUPERSONIC TURBULENT FLOW WITH LARGE DISTRIBUTED SURFACE INJECTION / /

ProvinceOrState

Illinois / New York / California / /

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