DEPENDENCE OF COMBUSTION CHAMBER RELIABILITY OF TURBOSHAFT AIRCRAFT ENGINE ON ITS GAS AND DYNAMIC PARAMETERS AND GEOMETRIC CHARACTERISTICS
A methodology for obtaining an empirical dependence which is used for determination of combustion chamber resource in turboshaft engines has been developed with the help of a plural linear regression method. Using this equation it is possible to determine combustion chamber resource with minimum tim...
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| Format: | Article |
| Language: | Russian |
| Published: |
Belarusian National Technical University
2006-10-01
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| Series: | Наука и техника |
| Online Access: | https://sat.bntu.by/jour/article/view/1239 |
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