11 research outputs found
An experimental investigation of the flow in a 1 1/2 stage axial turbine with regard to a high level of cooling-air injection
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An experimental investigation of the flow in a 1 1/2 stage axial turbine with regard to a high level of cooling-air injection
No full text
Clocking effects in a 1.5 stage axial turbine - steady and unsteady experimental investigations supported by numerical simulations
No full textNumerical investigation of vortex reducer flows in the high pressure compressors of modern aeroengines
No full textNumerical investigation of vortex reducer flows in the high pressure compressors of modern aeroengines
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