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The application of high inlet swirl angles for broad operating range turbocharger compressor

By A.H. Abdullah

Abstract

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN008436 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Topics: 21E - Jet turbine engines, gas turbine engines, 09L - Computer-Aided Design (CAD)
Year: 1996
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Provided by: OpenGrey Repository
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