INVESTIGATION OF THE EFFECT OF AIR HUMIDITY ON GAS TURBINE ENGINE PARAMETERS

The mathematical model of a turbo-shaft engine with a two-stage gas generator was obtained. This model is based on the multi-stage compressor blade – to - blade description, which makes it possible to evaluate the effect of air humidity on its performances. The characteristics of the axial multistag...

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Bibliographic Details
Main Authors: Людмила Георгиевна Бойко, Вадим Анатольевич Даценко
Format: Artigo
Language:Inglês
Published: National Aerospace University «Kharkiv Aviation Institute» 2017-11-01
Series:Авіаційно-космічна техніка та технологія
Subjects:
газотурбінний двигун
вологовміст
математична модель
осьовий багатоступеневий компресор
Online Access:http://nti.khai.edu/ojs/index.php/aktt/article/view/514
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