Spelling suggestions: "subject:"unsteady low (aerodynamics)"" "subject:"unsteady low (neurodynamics)""
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Velocity and temperature measurements in a non-premixed reacting flow behind a backward facing stepWu, Men-Zan B. 05 1900 (has links)
No description available.
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Unsteady pressure and inflow velocity on a pitching rotor blade in hoverLal, Mihir Kumar 12 1900 (has links)
No description available.
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An experimental investigation of the turbulent flow in the junction of a flat plate and a body of constant thicknessOguz, Ergün Abdullah 12 1900 (has links)
No description available.
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An implicit higher-order spatially accurate scheme for solving time dependent flows on unstructured meshesTomaro, Robert F. 12 1900 (has links)
No description available.
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A theory for the analysis of rotorcraft operating in atmospheric turbulenceCostello, Mark Francis 05 1900 (has links)
No description available.
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Turbulent boundary layers over rigid and moving wavy surfacesSengupta, Tapan Kumar 08 1900 (has links)
No description available.
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Numerical solutions of unsteady flow past rotor sectionsTang, Wei 08 1900 (has links)
No description available.
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A multi-resolution discontinuous galerkin method for unsteady compressible flowsShelton, Andrew Brian January 2008 (has links)
Thesis (Ph.D.)--Aerospace Engineering, Georgia Institute of Technology, 2009. / Committee Chair: Smith, Marilyn; Committee Co-Chair: Zhou, Hao-Min; Committee Member: Dieci, Luca; Committee Member: Menon, Suresh; Committee Member: Ruffin, Stephen
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Tip clearance and angle of attack effects upon the unsteady response of a vibrating flat plate in crossflow /Lewis, Daniel Joseph, January 1993 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1993. / Vita. Abstract. Includes bibliographical references (leaves 47-50). Also available via the Internet.
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Mathematical Model for Estimating Transient Pressure Surges in Cryogenic Liquid-Vapor SystemsPfister, Philippe 01 January 1983 (has links) (PDF)
Numerical treatments have become the most accurate methods for transient liquid flows analysis. Based on a computer code provided by NASA/KSC, this paper presents two simulations of cryogenic transfer systems. Experimental data originated from the Space Shuttle Liquid Oxygen Servicing were obtained during drain flows. Two sets of data (pressure at various locations versus time) corresponding to a drain stop and a drain initiation were used for a comparison with the predicted pressures. The first test case was a single-phase flow whereas the second one was associated with liquid-column separation and vapor cavity collapse. Major modifications were made to the computer program for two-phase flow treatments. Encouraging results have been obtained validating the model and opening new perspectives for future work.
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