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Oblique Shock Waves
1
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Flow separation in shock wave boundary layer interactions at hypersonic speeds


Hamed, A. (Awatef)
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]. 1990

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:4274    ---  Available
2
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Interactive calculation procedures for mixed compression inlets


Reshotko, Eli.
Cleveland, Ohio : Dept. of Mechanical and Aerospace Engineering, School of Engineering, Case Institute of Technology, Case Western Reserve University, [1983] 1983

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 Axe Federal Documents Online  NAS 1.26:186581    ---  Available
3
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Shock generation and control using DBD plasma actuators SBIR phase I final report


Patel, Mehul P., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] 2012

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:2012-217448    ---  Available
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