TURBOSHAFT ENGINE THERMOGASDYNAMIC PARAMETERS CALCULATION METHOD BLADE-TO BLADE DESCRIPTION TURBOMASHINES BASED. PART 1.MAIN EQUATIONS
Gas turbine engines processes mathematic simulations are widely used in different steps of its living cycle. All engine simulations may be divided into different difficulty levels: higher simulation level allows doing a more precise description of physical processes in main units of gas turbine eng...
Main Authors: | , , |
---|---|
Format: | Article |
Language: | English |
Published: |
National Aerospace University «Kharkiv Aviation Institute»
2018-02-01
|
Series: | Авіаційно-космічна техніка та технологія |
Subjects: | |
Online Access: | http://nti.khai.edu/ojs/index.php/aktt/article/view/29 |