Global ETD Search
Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.
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Showing 1 to 5 of 5 for “"shock reflections"”.
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Numerical Solution of Plane Viscous Shock Reflections
Made available in DSpace on 2014-12-09T22:17:27Z (GMT). No. of bitstreams: 1 6604289.pdf: 2394133 bytes, checksum: 41e29f0a83e0729fb70c97b229c41ac7 (MD5) Previous issue date: 1965
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Bifurcating Mach Shock Reflections with Application to Detonation Structure
Numerical simulations of Mach shock reflections have shown that the Mach stem can bifurcate as a result of the slip line jetting forward. Numerical simulations were conducted in this study which determined that these bifurcations occur when the Mach number is high, the ramp angle is high, and …
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Advancing Exhaust Flow Uniformity, Operational Stability, and Total Pressure Gain of Rotating Detonation Engines for Successful Turbine Integration
… involves several non-idealities, generating a shock-laden, highly unsteady exhaust flow field that differs substantially from steady, subsonic flow required at the turbine inlet.This dissertation aims to develop novel RDC designs with tailored inlet and exit geometries for successful turbine …
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Design and development of a continuous, open-return transonic wind tunnel facility
… such as compressible dynamic stall aerodynamics, shock buffet phenomenon and control, shock wave boundary layer ingestion to a propulsor, and other future research topics. The new wind tunnel is a rectangular testing facility with a 6 in (width) x 9 in (height) cross-sectional area in the test …
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Loss mechanisms in a highly loaded transonic axial turbine stage
… of blade profile loss, trailing edge loss, shock loss, endwall loss, secondary flow loss, tip leakage loss, cooling injection loss, and unsteady flow loss. The dominant sources of loss are determined to be the trailing edge loss, profile loss, and tip leakage loss. The computed flows show …