transonic - Globe Thesis

Keyword [transonic] Result: 181 - 200 \| Page: 10 of 10
181.	Influence of axial spacing on spanwise efficiency of a transonic axial compressor rotor stage
182.	Static and dynamic calibration of a multi-component sidewall force balance for a transonic Ludwieg tube wind tunnel
183.	Calculation of steady and unsteady transonic flow using a Cartesian mesh and gridless boundary conditions with application to aeroelasticity
184.	Effects of high intensity, large-scale freestream combustor turbulence on heat transfer in transonic turbine blades
185.	Aerodynamic loss modelling in transonic turbines
186.	Effects of inlet guide vane flow control on forced response of a transonic fan
187.	Enhanced inverse design code and development of design strategies for transonic compressor blading
188.	Fluid/structure coupled aeroelastic computations for transonic flows in turbomachinery
189.	An experimental and numerical investigation of stator-rotor interactions in a transonic compressor
190.	An improved streamline curvature approach for off-design analysis of transonic compression systems
191.	Transonic Flow Around Swept Wings: Revisiting Von Karman's Similarity Rule
192.	Transonic separated flow around a cavity
193.	Initial investigations of transonic turbine aerodynamics using the Carleton University High-Speed Wind Tunnel
194.	Numerical prediction of the interference drag of a streamlined strut intersecting a surface in transonic flow
195.	Transonic flow of moist air around thin airfoils
196.	A method for designing low-speed linear turbine cascades for the experimental investigation of viscous effects in transonic axial turbines
197.	Experimental investigation of two transonic linear turbine cascades at off-design conditions
198.	Efficient dynamic unstructured methods and applications for transonic flows and hypersonic stage separation
199.	Multistage interaction and transonic flow effects in a high-speed axial compressor
200.	Toward CFD-based correlations for a single-stage high-pressure transonic turbine
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