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Introduction of a tiltrotor aircraft service to the Atlanta air transportation marketMeyer, Stephen A. 08 1900 (has links)
No description available.
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Performance measurements, flow visualization, and numerical simulation of a crossflow fanSeaton, M. Scot. 03 1900 (has links)
Approved for public release, distribution unlimited / A 12-inch diameter, 1.5-inch span crossflow fan test apparatus was constructed and tested using the existing Turbine Test Rig (TTR) as a power source. Instrumentation was installed and a data acquisition program was developed to measure the performance of the crossflow fan. Performance measurements were taken over a speed range of 1,000 to 7,000 RPM. Results comparable to those measured by Vought Systems Division of LTV Aerospace in 1975 were obtained. At 6,000 RPM, a thrust-to-power ratio of one was determined; however, at 3,000 RPM twice the thrust-to-power ratio was measured. Flow visualization was conducted using dye-injection methods. Performance and flow visualization results were compared to predictions obtained from 2-D numerical simulation conducted using Flo++, a commercial PC-based computational fluid dynamics software package by Softflo. A possible design for a light civil V/STOL aircraft was suggested using a similar crossflow fan apparatus for both lift and propulsion. / Lieutenant, United States Navy
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Performance measurements, flow visualization, and numerical simulation of a crossflow fan /Seaton, M. Scot. 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. 69-70). Also available online.
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Vertical-take-off aircraft and long-range urban planning considerationsHunziker, Walter Rudolph 05 1900 (has links)
No description available.
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Experimental and numerical analysis of a crossflow fan /Cheng, Wee Teck. January 2003 (has links) (PDF)
Thesis (M.S. in Mechanical Engineering)--Naval Postgraduate School, December 2003. / Thesis advisor(s): Garth V. Hobson, Max F. Platzer. Includes bibliographical references (p. 83). Also available online.
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An experimental investigation of the vortices and the wake associatied with a jet in crossflowAntani, Dharmanshu Laxmilal 08 1900 (has links)
No description available.
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Aeroelastic and aeroacoustic modelling of rotorcraft /Opoku, Daniel G. January 1900 (has links)
Thesis (M.App.Sc.) - Carleton University, 2002. / Includes bibliographical references (p. 112-122). Also available in electronic format on the Internet.
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Transitions between hover and level flight for a tailsitter UAV /Osborne, Stephen R., January 2007 (has links) (PDF)
Thesis (M.S.)--Brigham Young University. Dept. of Electrical and Computer Engineering, 2007. / Includes bibliographical references (p. 77-78).
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Investigation of a stop-fold tiltrotorBosworth, Jeff. January 2009 (has links)
Thesis (M. S.)--Aerospace Engineering, Georgia Institute of Technology, 2010. / Committee Chair: Hodges, Dewey; Committee Member: Bauchau, Olivier; Committee Member: Sankar, Lakshmi. Part of the SMARTech Electronic Thesis and Dissertation Collection.
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Design and integration of an unmanned aerial vehicle navigation systemDittrich, Joerg S. 05 1900 (has links)
No description available.
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