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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 57 (0.075 seconds)Spelling suggestions: "subject:"unsteady flow (aerodynamics)"" "subject:"unsteady flow (neurodynamics)""
| 1 |
Turbulence modelling of unsteady separated flow over an airfoilStockdill, Barton Thomas. 10 April 2008 (has links)
No description available.
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| 2 |
Aerodynamics of nonrigid bodies undergoing large amplitude time-dependent motionsSingh, Jatinder 08 1900 (has links)
No description available.
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| 3 |
A study of the aerodynamic performance of Weis-Fogh wingsChen, Hsun Hu 05 1900 (has links)
No description available.
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| 4 |
Turbulence generated pressure fluctuations in a class of interior flowsHegde, Uday Gajanan 08 1900 (has links)
No description available.
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| 5 |
High speed aerodynamics of upper surface blowing aircraft configurationsBirckelbaw, Larry Dean 05 1900 (has links)
No description available.
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| 6 |
Study of turbulent flow in a wing-fuselage type junctureKubendran, Lagudua R. 05 1900 (has links)
No description available.
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| 7 |
Measurement of pressure-velocity correlations in turbulent reacting flowsKomerath, Narayanan Menon 08 1900 (has links)
No description available.
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| 8 |
Analysis of pressure gradient-velocity correlation in turbulent, premixed flamesChandran, Subhash B. S. 08 1900 (has links)
No description available.
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| 9 |
Analysis of a simplified nonlinear ground resonance modelJanowski, Michael David 12 1900 (has links)
No description available.
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| 10 |
An experimental and numerical investigation of a turbulent round jet issuing into an unsteady crossflow /Xia, Liping. January 1998 (has links)
Thesis (Ph. D.)--University of Hong Kong, 1998. / Includes bibliographical references (leaves 165-170).
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