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 |
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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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| _version_ | 1846146290598019072 |
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| author | D. N. Mironov |
| author_facet | D. N. Mironov |
| author_sort | D. N. Mironov |
| collection | DOAJ |
| description | 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 %. |
| format | Article |
| id | doaj-art-4aecca14150740f593a6b4f27626a1f6 |
| institution | Kabale University |
| issn | 2227-1031 2414-0392 |
| language | Russian |
| publishDate | 2006-10-01 |
| publisher | Belarusian National Technical University |
| record_format | Article |
| series | Наука и техника |
| spelling | doaj-art-4aecca14150740f593a6b4f27626a1f62024-12-02T03:58:14ZrusBelarusian National Technical UniversityНаука и техника2227-10312414-03922006-10-0105384110.21122/2227-1031-2006-0-5-38-411165DEPENDENCE OF COMBUSTION CHAMBER RELIABILITY OF TURBOSHAFT AIRCRAFT ENGINE ON ITS GAS AND DYNAMIC PARAMETERS AND GEOMETRIC CHARACTERISTICSD. N. Mironov0Belarusian National Technical UniversityA 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 %.https://sat.bntu.by/jour/article/view/1239 |
| spellingShingle | D. N. Mironov DEPENDENCE OF COMBUSTION CHAMBER RELIABILITY OF TURBOSHAFT AIRCRAFT ENGINE ON ITS GAS AND DYNAMIC PARAMETERS AND GEOMETRIC CHARACTERISTICS Наука и техника |
| title | DEPENDENCE OF COMBUSTION CHAMBER RELIABILITY OF TURBOSHAFT AIRCRAFT ENGINE ON ITS GAS AND DYNAMIC PARAMETERS AND GEOMETRIC CHARACTERISTICS |
| title_full | DEPENDENCE OF COMBUSTION CHAMBER RELIABILITY OF TURBOSHAFT AIRCRAFT ENGINE ON ITS GAS AND DYNAMIC PARAMETERS AND GEOMETRIC CHARACTERISTICS |
| title_fullStr | DEPENDENCE OF COMBUSTION CHAMBER RELIABILITY OF TURBOSHAFT AIRCRAFT ENGINE ON ITS GAS AND DYNAMIC PARAMETERS AND GEOMETRIC CHARACTERISTICS |
| title_full_unstemmed | DEPENDENCE OF COMBUSTION CHAMBER RELIABILITY OF TURBOSHAFT AIRCRAFT ENGINE ON ITS GAS AND DYNAMIC PARAMETERS AND GEOMETRIC CHARACTERISTICS |
| title_short | DEPENDENCE OF COMBUSTION CHAMBER RELIABILITY OF TURBOSHAFT AIRCRAFT ENGINE ON ITS GAS AND DYNAMIC PARAMETERS AND GEOMETRIC CHARACTERISTICS |
| title_sort | dependence of combustion chamber reliability of turboshaft aircraft engine on its gas and dynamic parameters and geometric characteristics |
| url | https://sat.bntu.by/jour/article/view/1239 |
| work_keys_str_mv | AT dnmironov dependenceofcombustionchamberreliabilityofturboshaftaircraftengineonitsgasanddynamicparametersandgeometriccharacteristics |