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  • About
  • The Global ETD Search service is a free service for researchers to find electronic theses and dissertations. This service is provided by the Networked Digital Library of Theses and Dissertations.
    Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
211

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.
212

Viscous modeling of ground effect aerodynamics of airfoil and jet

Ockfen, 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).
213

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.
214

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.
215

Hot-wire surveys in the vortex wake downstream of a three-percent fighter aircraft model at high angles of attack

Frink, 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.
216

Theory and practice of flutter calucations for systems with many degrees of freedom

Vooren, Adriaan Isak van de. January 1900 (has links)
Proefschrift - Technische Hoogeschool Delft. / "Stellingen": 4 p. inserted. Bibliography: p. [99]-100.
217

On the airflow past a heated sphere

Hartmann, 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.
218

Interactions of coherent structures in annular jets /

Lau, Kwok-keung. January 1991 (has links)
Thesis (Ph. D.)--University of Hong Kong, 1992.
219

A flow visualization study of LEX generated vortices on a scale model of F/A-18 fighter aircraft at high angles of attack

Cavazos, 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.
220

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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