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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.
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Showing 1 to 10 of 13 (0.07 seconds)Spelling suggestions: "subject:"propellers, periferial"" "subject:"propellersogs, periferial""
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The static thrust characteristics of a propeller with trailing-edge flapsDutton, D. W. (Donnell Wayne) 05 1900 (has links)
No description available.
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| 2 |
The performance of propellers operating at zero advance ratio.Gilmore, David Cunningham. January 1967 (has links)
No description available.
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| 3 |
Jet propulsion experimentsHarper, John Joseph 05 1900 (has links)
No description available.
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| 4 |
Design of propeller shrouds for static thrust conditions by method of singularitiesGappa, Joseph Anthony 12 1900 (has links)
No description available.
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| 5 |
Theoretical investigation of jet propulsionWilson, Robert E. (Robert Elmer) 05 1900 (has links)
No description available.
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| 6 |
Vertical ascent analysis of the lifting airscrewFagan, Robert Harvard 05 1900 (has links)
No description available.
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| 7 |
The performance of propellers operating at zero advance ratio.Gilmore, David Cunningham. January 1967 (has links)
No description available.
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| 8 |
An efficient hybrid scheme for the solution of rotational flow around advanced propellersSrivastava, Rakesh 08 1900 (has links)
No description available.
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| 9 |
Propeller performance analys and multidisciplinary optimization using a genetic algorithmBurger, Christoph, Hartfield, Roy J., January 2007 (has links) (PDF)
Thesis (Ph. D.)--Auburn University, 2007. / Abstract. Vita. Includes bibliographical references.
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| 10 |
Integrating matrix method for determining the natural vibrations of a rotating, unsymmetrical beam with application to twisted propeller bladesHunter, William Francis January 1967 (has links)
A numerical method is presented for determining the natural vibration frequencies, and the corresponding mode shapes, of a rotating cantilever beam which has a nonuniform, unsymmetrical cross section. Two coupled fourth-order differential equations of motion with variable coefficients are derived which govern the motion of such a beam having deformations in two directions. Through the development and utilization of the integrating matrix, the solution of the differential equations is obtained in the form of an eigenvalue problem. The solutions to the eigenvalue problem are determined by an iteration method based upon a special orthogonality relationship which is derived. Numerical examples, including an application to a twisted propeller blade, are presented with the results of the integrating matrix solutions being compared to exact solutions and experimental data. / Master of Science
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