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Cycle analysis for helicopter gas turbine engines

By A.D Bewley and Farnborough (United Kingdom) Royal Aerospace Establishment

Abstract

SIGLEAvailable from British Library Document Supply Centre- DSC:8670.19(RAE-TM-P--1154) / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Topics: 21E - Jet turbine engines, gas turbine engines, 01C - Aircraft, aircraft components, Cycle analysis for helicopter gas turbine engines [ Thermodynamic cycles]
Year: 1989
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Provided by: OpenGrey Repository
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