- About
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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.
Search results
Showing 1 to 10 of 40 (0.062 seconds)| 1 |
The analysis of wing loads in roller coaster maneuversRees, Pembroke Graves 08 1900 (has links)
No description available.
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A methodology for robust structural design with application to active aeroelastic wingsZink, Paul Scott 08 1900 (has links)
No description available.
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Optimal lifting surfaces, including end plates, ground effect & thickness / David William Fin Standingford.Standingford, David William Fin January 1997 (has links)
Bibliography: leaves 164-172. / xii, 172 leaves : ill. (some col.) ; 30 cm. / Title page, contents and abstract only. The complete thesis in print form is available from the University Library. / The task of calculating the aerodynamic load distribution on a thin three-dimensional lifting surface or wing of finite aspect ratio at small angle of attack presents difficulties for most numerical methods. The two-dimensional lifting-surface integral equation that must be solved is highly singular, and does not possess analytic solutions, even for simple plan-form geometries such as rectangles or ellipses. / Thesis (Ph.D.)--University of Adelaide, Dept. of Applied Mathematics, 1998
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Optimal lifting surfaces, including end plates, ground effect & thickness / David William Fin Standingford.Standingford, David William Fin January 1997 (has links)
Bibliography: leaves 164-172. / xii, 172 leaves : ill. (some col.) ; 30 cm. / Title page, contents and abstract only. The complete thesis in print form is available from the University Library. / The task of calculating the aerodynamic load distribution on a thin three-dimensional lifting surface or wing of finite aspect ratio at small angle of attack presents difficulties for most numerical methods. The two-dimensional lifting-surface integral equation that must be solved is highly singular, and does not possess analytic solutions, even for simple plan-form geometries such as rectangles or ellipses. / Thesis (Ph.D.)--University of Adelaide, Dept. of Applied Mathematics, 1998
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Optimal lifting surfaces, including end plates, ground effect & thickness /Standingford, David William Fin. January 1997 (has links) (PDF)
Thesis (Ph. D.)--University of Adelaide, Dept. of Applied Mathematics, 1998. / Includes bibliographical references (leaves 164-172).
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An investigation of a method for determining the pressure distribution on an accelerating flat plate at an angle of attack at hypersonic or supersonic velocitiesHannon, Clarence William 08 1900 (has links)
No description available.
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Airloads on a finite wing in a time dependent incompressible freestreamGillam, David A. 08 1900 (has links)
No description available.
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The effects of nonstationary aerodynamics on the rigid-body dynamic stability of an airplaneStatler, Irving C. January 1956 (has links)
Thesis--California Institute of Technology. / Includes bibliographical references.
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The effects of nonstationary aerodynamics on the rigid-body dynamic stability of an airplaneStatler, Irving C. January 1956 (has links)
Thesis--California Institute of Technology. / Includes bibliographical references.
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Stability of cylindrical laminates by highter order shear deformable theoriesAnastasiadis, John S. 12 1900 (has links)
No description available.
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