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Interactive calculation of cross-sectional areas for aircraft design and analysis /Grieshaber, Michele Marie, January 1988 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1988. / Vita. Abstract. Includes bibliographical references (leaves 54-55). Also available via the Internet.
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Viscous modeling of ground effect aerodynamics of airfoil and jetOckfen, Alex Earle, January 2008 (has links) (PDF)
Thesis (M.S. in mechanical engineering)--Washington State University, December 2008. / Title from PDF title page (viewed on Dec. 31, 2008). "School of Mechanical and Materials Engineering." Includes bibliographical references (p. 149-154).
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Control power requirements for the velocity vector roll /Ashley, Patrick A. January 1994 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1994. / Vita. Abstract. Includes bibliographical references (leaf 48). Also available via the Internet.
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An experimental study of a turbulent wing-body junction and wake flow /Fleming, Jonathan Lee, January 1991 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1991. / Vita. Abstract. Includes bibliographical references (leaves 108-112). Also available via the Internet.
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Hot-wire surveys in the vortex wake downstream of a three-percent fighter aircraft model at high angles of attackFrink, William D. January 1990 (has links) (PDF)
Thesis (M.S. in Engineering Science)--Naval Postgraduate School, December 1990. / Thesis Advisor(s): Hebbar, Sheshagiri K. ; Platzer, Max F. "December 1990." Description based on title screen as viewed on March 31, 2010. DTIC Identifier(s): Trailling Vortices, Wake, Trubulent Flow, Jet Fighters, High Alpha (High Angle of Attack), Vortex Wake, Angle of Attack, Extendable Structures, Leading Edges, Fences, Lex Fences, Wind Tunnel Models, F-17 Aircraft, F/A-18 Aircraft, Wind Tunnel Tests, Hot Wire Anemometers, Theses. Author(s) subject terms: High Angle-of-Attack Aerodynamics, Hot-Wire Measurements, Wind Tunnel Studies. Includes bibliographical references (p. 24-25). Also available in print.
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Theory and practice of flutter calucations for systems with many degrees of freedomVooren, Adriaan Isak van de. January 1900 (has links)
Proefschrift - Technische Hoogeschool Delft. / "Stellingen": 4 p. inserted. Bibliography: p. [99]-100.
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On the airflow past a heated sphereHartmann, Irving. January 1934 (has links)
Thesis (Ph. D.)--Catholic University of America, 1935. / "Reprinted from the Journal of the Franklin institute, vol. 218, no. 5, November, 1934." Bibliography: p. 20.
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Interactions of coherent structures in annular jets /Lau, Kwok-keung. January 1991 (has links)
Thesis (Ph. D.)--University of Hong Kong, 1992.
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A flow visualization study of LEX generated vortices on a scale model of F/A-18 fighter aircraft at high angles of attackCavazos, Odilon V. January 1990 (has links) (PDF)
Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, June 1990. / Thesis Advisor(s): Hebbar, S. K. ; Platzer, M. F. "June 1990." Description based on title screen as viewed on October 19, 2009. DTIC Descriptor(s): Angles, yaw, scale models, attack, motion, rates, moments, vortices, flow visualization, rupture, asymmetry, aerodynamic forces, leading edges, range(distance), statics, hysteresis, aerodynamics, high angles, pitch(motion). DTIC Indicator(s): Flow visualization, trailing vortices, F/A-18 aircraft. Author(s) subject terms: High angle of attack aerodynamics, effect of pitch rate and yaw, vortex development and bursting, flow visualization by dye injection, water tunnel studies, F/A-18 fighter aircraft. Includes bibliographical references (p. 44-45). Also available in print.
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An experimental and computational aerodynamic investigation of a low-canard high-wing aircraft design /Mazza, Joseph R., January 1993 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1993. / Vita. Abstract. Includes bibliographical references (leaf 28). Also available via the Internet.
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