DEPENDENCE OF COMBUSTION CHAMBER RELIABILITY OF TURBOSHAFT AIRCRAFT ENGINE ON ITS GAS AND DYNAMIC PARAMETERS AND GEOMETRIC CHARACTERISTICS

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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Veröffentlicht in:Nauka i tekhnika (Minsk, Belarus : 2012) Belarus : 2012), 2006-10 (5), p.38-41
1. Verfasser: D. N. Mironov
Format: Artikel
Sprache:rus
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Zusammenfassung: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 time, intellectual and material expenses and with an error order of 5 %.
ISSN:2227-1031
2414-0392
DOI:10.21122/2227-1031-2006-0-5-38-41