Gas Turbine Laboratory: Recent submissions
Now showing items 100-102 of 123
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Prediction of three-dimensional compressible turbulent boundary layers on transonic compressor blades
(c1980, c1980)A small crossflow approximation to the full three dimensional compressible turbulent boundary layer equations for turbomachine blade rows is developed by taking advantage of the nature of blade geometry and inviscid flow ... -
Experiments on turbulent boundary layers along a circular cylinder with and without separation
(Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1967], 1967)Summary: Experiments were conducted in a turbulent boundary-layer near separation along a circular cylinder with the flow in the axial direction. The pressure gradient along the axis of the cylinder could be varied such ... -
Detailed time resolved measurements and analysis of unsteady flow in a transonic compressor
(c1980, c1980)Detailed time and space resolved measurements for a transonic compressor stage have been completed in the MIT Blowdown Compressor Facility. The stage studied was a new first stage for a NASA two-stage machine which ...
