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Design and testing of a combustor for a turbo-ramjet for UAV and missile applications /Piper, Ross H. January 2003 (has links) (PDF)
Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, March 2003. / Thesis advisor(s): Garth V. Hobson, Raymond P. Shreeve. Includes bibliographical references (p. 81-82). Also available online.
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Numerical investigation of wing morphing capabilities applied to a Horten type swept wing geometryVishwanathan, Ashwin. January 2007 (has links)
Thesis (M.S.)--West Virginia University, 2007. / Title from document title page. Document formatted into pages; contains viii, 58 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 51-52).
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Improvement of the performance of a turbo-ramjet engine for UAV and missile applications /Krikellas, Dimitrios. January 2003 (has links) (PDF)
Thesis (M.S. in Applied Physics and M.S. in Aeronautical Engineering)--Naval Postgraduate School, December 2003. / Thesis advisor(s): Garth V. Hobson, Kai E. Woehler. Includes bibliographical references (p. 133). Also available online.
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A CFD/CSD interaction methodology for aircraft wings /Bhardwaj, Manoj K. January 1997 (has links)
Thesis (Ph. D.)--Virginia Polytechnic Institute and State University, 1997. / Vita. Includes bibliographical references (p. 115-121).
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Development of conjugate heat transfer capability to an unstructured flow solver - U²NCLEXue, Qingluan, January 2005 (has links)
Thesis (M.S.) -- Mississippi State University. Computational Engineering. / Title from title screen. Includes bibliographical references.
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Transport and dispersion of fire extinguishing agents downstream from clutter elements of aircraft engine nacellesUnknown Date (has links)
The combination of highly turbulent airflow, flammable fluids, and numerous ignition sources makes aircraft engine nacelles a difficult fire zone to protect. Better understanding of nacelle air flow and how it influences the spread of fires and fire extinguishing agents is needed to improve the efficiency of fire suppression. The first objective was to establish a CFD model for a flow field test section to analyze the transport and dispersion of fire extinguishing agents in the presence of various clutter elements. To validate the use of the CFD model, the simulation results of the CFD model were compared to the experimental data and they show an agreement with the experimental data. The second objective was to present parametric studies to show the effects of the coflow speed, turbulence intensity and agent droplet size on the transport and dispersion of the agent particles downstream from the clutter elements. / by Khaled Zbeeb. / Thesis (M.S.C.S.)--Florida Atlantic University, 2009. / Includes bibliography. / Electronic reproduction. Boca Raton, Fla., 2009. Mode of access: World Wide Web.
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