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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 546 (0.03 seconds)| 1 |
Three-dimensional numerical simulation of a supersonic under-expanded rectangular jetAl-Qadi, Ibraheem M. A. , January 2003 (has links)
Thesis (Ph. D.)--Ohio State University, 2003. / Title from first page of PDF file. Document formatted into pages; contains xix, 147 p; also contains graphics (some col.). Includes bibliographic references. Available online via OhioLINK's ETD Center.
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A variational calculation of the trapping current in a thermal barrierLi, Xing Zhong. January 1983 (has links)
Thesis (Ph. D.)--University of Wisconsin--Madison, 1983. / Typescript. Vita. eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references (leaves 77-78).
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Kinetic analysis of the thermal barrier in a tandem mirrorCarrera, Rodolfo. January 1983 (has links)
Thesis (Ph. D.)--University of Wisconsin--Madison, 1983. / Typescript. Vita. eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references.
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Time dependent studies of a tandem mirror with thermal barriersMontalvo, Elena. January 1983 (has links)
Thesis (Ph. D.)--University of Wisconsin--Madison, 1983. / Typescript. Vita. eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references.
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Aerodynamic drag of ridge arrays in adverse pressure gradientsAbd Rabbo, M. F. January 1976 (has links)
Drag measurements for excrescence arrays of square section mounted on a smooth wall and subjected to two adverse pressure gradients in equilibrium are obtained. Differences in drag which arise when the excrescences are uniformly distributed and when tending to isolation are shown. Flow visualization photographs using the surface oil flow technique are presented to illustrate different flow patterns around arrays of varying spacing. A prediction model for the drag of excrescence arrays based on the results obtained was devised. Its range of application could be extended to excrescences of varying shape providing they are sufficiently small to be immersed in the logarithmic part of the boundary layer. Drag results are determined by both a momentum defect and a pressure distribution technique. These results are compared and the difference between them is partially attributed to the change in surface friction between the excrescences and partially to some lack of two-dimensionality in the test procedure. Corrections for the latter effect are made to the data obtained.
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The sound of moving bodiesBrentner, Kenneth Steven January 1990 (has links)
No description available.
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Far - field boundaries and their numerical treatmentKarni, S. January 1989 (has links)
No description available.
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Aerodynamic and aeroacoustic estimations of oscillatory supersonic flowsRona, Aldo January 1997 (has links)
No description available.
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The aerodynamic drag of high speed trainsBrockie, N. J. W. January 1988 (has links)
No description available.
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Prediction of induced rolling moments in slender cruciform canard controlled configurations at moderately high angles of attackGnanasekaran, V. January 1981 (has links)
No description available.
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