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Stability properties of two-dimensional sail configurations.Haselgrove, Maxwell Keith. January 1973 (has links) (PDF)
Thesis (Ph.D. 1973) from the Dept. of Applied Mathematics, University of Adelaide.
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Sjømann og handverker Seilmakere ved Oslofjorden og Skagerrak, 1850-1914 /Berggreen, Brit. January 1973 (has links)
Originally presented as the author's Thesis (M.A.), Oslo, 1972. / Includes bibliographical references (p. 126-128).
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Investigation of the forces developed by a yacht sailBarrett, Peter Jones. January 1962 (has links)
Thesis (M.S.)--University of Wisconsin--Madison, 1962. / Typescript. eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references (leaf 72).
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Battens for two-dimensional sails with prescribed pressure distributions / Battens for 2-dimensional sails with prescribed pressure distributions.Ugolini, Bruno. January 1987 (has links)
No description available.
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Battens for two-dimensional sails with prescribed pressure distributionsUgolini, Bruno. January 1987 (has links)
No description available.
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Stability properties of two-dimensional sail configurationsHaselgrove, Maxwell Keith January 1973 (has links)
iii, 120 leaves : ill. / Title page, contents and abstract only. The complete thesis in print form is available from the University Library. / Thesis (Ph.D.1973) from the Dept. of Applied Mathematics, University of Adelaide
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Design of optimal cyclers using solar sails /Stevens, Robert E. January 2002 (has links) (PDF)
Thesis (Aeronautical and Astronautical Engineer)--Naval Postgraduate School, December 2002. / Thesis advisor(s): I. Michael Ross, Dennis Byrnes. Includes bibliographical references (p. 119-120). Also available online.
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Thermal analysis and thermal control system requirements for a solar sail Mars mission /Tiedemann, Maik, January 1991 (has links)
Report (M. Eng.)--Virginia Polytechnic Institute and State University, 1991. / Vita. Abstract. Includes bibliographical references (leaves 75-76). Also available via the Internet.
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Three-dimensional viscous flow analysis of tip-sail effects on wing performance at low reynolds numbersFerley, Dean 12 September 2015 (has links)
Steady, three-dimensional viscous numerical analysis of airflow over a rectangular NACA 0012 base wing (BW) with a rounded tip and with three NACA 0015 tip-sails (WTS) is performed. The flow physics and aerodynamic forces are studied at Reynolds numbers (Re) of 60,000 and 600,000, angles of attack (α) of 0, 5, 7.5, and 10°, and two sets of tip-sail dihedral angles (leading to trailing tip-sail): 50, 45, and 40° and 60, 45, and 30°. The Shear Stress Transport turbulence and intermittency-transition Reynolds number transitional turbulence models were used. For α > 0°, the WTS produced higher lift coefficients (CL) and drag coefficients (CD) than the BW. At Re = 600,000 and α > 0°, the CL/CD was higher for the WTS than the BW. Good agreement was seen with experimental data at Re = 600,000 for the BW results and the WTS CL but not the WTS CD. / October 2015
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A solar sail technology application mission for analyzing the earth's geomagnetic tail /Prodger, David C. January 1900 (has links)
Thesis (M.App.Sc.) - Carleton University, 2002. / Includes bibliographical references (p. 124-130). Also available in electronic format on the Internet.
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