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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 48 (0.042 seconds)Spelling suggestions: "subject:"each number"" "subject:"nach number""
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A computational and analytical study of sound emitted by free shear flowsAvital, Eldad January 1998 (has links)
No description available.
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| 2 |
An investigation of aerodynamic controls at hypersonic Mach numbers /Fiore, Anthony William January 1967 (has links)
No description available.
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| 3 |
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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| 4 |
Solutions to the Navier-Stokes Equations in a Non-Inertial Reference FrameMajety, Kishore Satya 13 December 2003 (has links)
A general rotating frame formulation of the Navier-Stokes equations has been added to the incompressible and arbitrary Mach number versions of UNCLE. While eliminating the need for moving grids, this formulation also reduces the error caused by linear approximations of rotational motion. The formulation is validated for single axis rotations by comparing the simulations of a marine propeller and an isolated helicopter rotor with experimental data. A simulation of the helicopter rotor in pitching motion is also performed. Results are compared between the non-inertial reference frame formulation and absolute frame solver for a prolate spheroid with all the components of angular velocity. The use of the non-inertial reference frame promises a faster and more accurate six-degree-ofreedom simulations.
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| 5 |
Theoretical and experimental study of equilibrium and non-equilibrium air flow through a Mach number 10 contoured nozzle /Zonars, Demetrius Constantine January 1965 (has links)
No description available.
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| 6 |
Experimental and numerical studies of S-shaped diffusing ductsOng, Lih-Yenn January 1997 (has links)
No description available.
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| 7 |
A study of transonic normal shock wave-turbulent boundary layer interactions in axisymmetric internal flow /Om, Deepak. January 1982 (has links)
Thesis (Ph. D.)--University of Washington, 1982. / Vita. Includes bibliographical references.
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| 8 |
Modeling dynamic stall of SC-1095 airfoil at high mach numberClark, Brian 26 January 2010 (has links)
In this thesis, the Leishman-Beddoes method of determining airloads for
an airfoil undergoing dynamic stall is studied over a range of Mach numbers. To
validate the method for conditions where little experimental data is available, a
computational fluid dynamics solver is utilized to provide airload predictions for
comparison to the Leishman-Beddoes results.
It is found that even for high Mach numbers the Leishman-Beddoes
method provides reliable predictions for lift coefficient. However, at the higher
Mach numbers pitching moment is sometimes overpredicted at high angle of
attack. This is seemingly due to an inability to accurately determine the center of
pressure in the high speed unsteady flow environment.
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| 9 |
Design and analysis of rocket nozzle contours for launching pico-satellites /Denton, Brandon Lee. January 2008 (has links)
Thesis (M.S.)--Rochester Institute of Technology, 2008. / Typescript. Includes bibliographical references (leaves 110-111).
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| 10 |
Influence of loading distribution on the performance of high pressure turbine blades /Corriveau, Daniel, January 1900 (has links)
Thesis (Ph.D.) - Carleton University, 2005. / Includes bibliographical references (p. 295-301). Also available in electronic format on the Internet.
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