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Application to supersonic diffusers of a one-dimensional fluid flow equation of the Pfaffian typePinckney, S. Z. January 1963 (has links)
Master of Science
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Aspirating probes for measurement of mean concentration and fluctuating quantities in supersonic air/helium shear layerNinnemann, Todd A. 23 December 2009 (has links)
Two aspirating hot-film probes are developed to make measurements in supersonic air/helium shear layers. The first probe is designed to measure local mean gas composition and is referred to as the mean concentration probe. This probe consists of a constant temperature hot-film sensor operating in a channel with a choked exit. The flow over the hot-fifm is influenced only by total temperature, total pressure, and gas composition. The mean probe is easily calibrated and shows acceptable sensitivity to flow angularity. The second probe is based on an improved design of the mean concentration probe. In addition to measuring mean composition, this second probe also measures turbulence intensities of Reynolds number and thermal conductivity using a multiple overheat method. This probe is referred to as the turbulent probe. Both probes are used in the study of supersonic air/helium mixing layers in the VPI&SU 23 cmx23 cm Supersonic Wind Tunnel. Profiles of mean and turbulent quantities are presented. / Master of Science
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Some problems in the numerical modelling of the lower stratosphereJones, Anna Elizabeth January 1993 (has links)
No description available.
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BOUNDARY LAYERS IN MAGNETOGASDYNAMICS WITH PRESSURE GRADIENT AND HEAT TRANSFERSpring, Francis Edward, 1941- January 1968 (has links)
No description available.
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The supersonic transport development program: a case study of the impact of technology upon the socio-political environmentBarish, Lawrence Stephen, 1945- January 1970 (has links)
No description available.
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An investigation of a method for determining the pressure distribution on an accelerating flat plate at an angle of attack at hypersonic or supersonic velocitiesHannon, Clarence William 08 1900 (has links)
No description available.
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The effect of superheat on liquid droplets in a supersonic freestream.Newman, Aaron W. January 1999 (has links) (PDF)
Thesis (M.S.)--Worcester Polytechnic Institute. / Keywords: droplet injection; supersonic crossflow; superheat; droplet disruption. Includes bibliographical references (leaves 72-75).
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Fan noise reduction from a supersonic inlet /Nuckolls, William E., January 1992 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1992. / Vita. Abstract. Includes bibliographical references (leaves 66-67). Also available via the Internet.
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Detection and measurement of density fluctuations induced by a magnetohydrodynamic force in a supersonic boundary layerCundy, Michael E. January 2005 (has links)
Thesis (Honors)--Ohio State University, 2005. / Title from first page of PDF file. Document formatted into pages; contains 29 p.; also includes graphics (some col.). This research has been supported by the AFOSR under grant F49620-02-1-0164, Phase II SBIR grant F33615-01-C-3112 of Air Vehicles Directorate of AFRL, and by the National Science Foundation (NSF) Division of Plasma Physics. Available online via Ohio State University's Knowledge Bank. Includes bibliographical references (p. 29). Available online via Ohio State University's Knowledge Bank.
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Interaction of microwave filaments and blunt body in supersonic flowFarzan, Farnaz. January 2008 (has links)
Thesis (M.S.)--Rutgers University, 2008. / "Graduate Program in Mechanical and Aerospace Engineering." Includes bibliographical references (p. 71-73).
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