Formulas of reducing engine environmental performance and combustion characteristics to standard atmospheric conditions
The article specifies formulas of reducing environmental performance and combustion characteristics of a gas turbine engine, as well as its thermodynamic parameters to the standard atmospheric conditions, with flight altitude H = 0 and Mach number M = 0: p0= 760 mm Hg. (101.325 kPa), T0=288.15 K (+1...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Samara National Research University
2017-07-01
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| Series: | Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение |
| Subjects: | |
| Online Access: | https://journals.ssau.ru/vestnik/article/viewFile/5115/5002 |