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Aviation / Space technology / Aerodynamics / Aircraft engines / Single-stage-to-orbit / Scramjet / Ramjet / Hypersonic speed / Combustor / Aerospace engineering / Jet engines / Spacecraft propulsion


ANALYSIS AND DESIGN OF A HYPERSONIC SCRAMJET ENGINE WITH A STARTING MACH NUMBER OF 4.00 by
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Document Date: 2014-01-20 16:06:48


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File Size: 2,80 MB

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City

Charlotte / /

Facility

MASTER OF SCIENCE IN AEROSPACE ENGINEERING THE UNIVERSITY OF TEXAS AT ARLINGTON August / MS The University of Texas / The University of Texas / /

Organization

Federal Aviation Administration / Department of Mechanical and Aerospace Engineering / Graduate School / University of Texas at Arlington / Aerodynamics Research Center / AVD Lab / Air Force / /

Person

Amit Oza / Wilbur Wright / Bernd Chudoba / Jennifer / Xiao Huang / Brad Mixon / Calvin Reasoner / Rick Wild / Bob Mullins / Charlotte / Philip Panicker / Melissa / Bryan Mixon / Vicki Andrews / Kent Lawrence / Betty Reasoner / Sarah / Andrea / Lacy / KRISTEN NICOLE ROBERTS / Russ Davoren / Scott Kordis / Nauman Mhaskar / Gary Coleman / Carissa / Donald Wilson / Paul iii / Frank Lu / Roger Goolsby / Steve Andrews / /

Position

research advisor / Graduate Teaching Assistant / excellent professor / /

ProvinceOrState

Texas / /

Technology

existing technology / /

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