An Estimate of the Influence of the Compressor Stability Margin on the Pick-Up Time of a Turbojet Engine
The relations are derived enabling to estimate the acceleration time of the turbojet engine rotor set. The terms are established allowing for the determination of the effect of individual operational and structural engine parameters upon the time needed for acceleration of the rotor system. Influen...
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| Format: | Article |
| Language: | English |
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Institute of Fundamental Technological Research
1991-07-01
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| Series: | Engineering Transactions |
| Online Access: | https://et.ippt.pan.pl/index.php/et/article/view/1622 |
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| _version_ | 1839633434399473664 |
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| author | M. Orkisz |
| author_facet | M. Orkisz |
| author_sort | M. Orkisz |
| collection | DOAJ |
| description |
The relations are derived enabling to estimate the acceleration time of the turbojet engine rotor set. The terms are established allowing for the determination of the effect of individual operational and structural engine parameters upon the time needed for acceleration of the rotor system. Influence of the economic and optimum ranges of operation upon that time is also analyzed.
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| format | Article |
| id | doaj-art-a48f87e1af984fa898b9a8e9068e93a3 |
| institution | Matheson Library |
| issn | 0867-888X 2450-8071 |
| language | English |
| publishDate | 1991-07-01 |
| publisher | Institute of Fundamental Technological Research |
| record_format | Article |
| series | Engineering Transactions |
| spelling | doaj-art-a48f87e1af984fa898b9a8e9068e93a32025-07-11T04:56:15ZengInstitute of Fundamental Technological ResearchEngineering Transactions0867-888X2450-80711991-07-01392An Estimate of the Influence of the Compressor Stability Margin on the Pick-Up Time of a Turbojet EngineM. Orkisz0Air Force Academy, Dęblin The relations are derived enabling to estimate the acceleration time of the turbojet engine rotor set. The terms are established allowing for the determination of the effect of individual operational and structural engine parameters upon the time needed for acceleration of the rotor system. Influence of the economic and optimum ranges of operation upon that time is also analyzed. https://et.ippt.pan.pl/index.php/et/article/view/1622 |
| spellingShingle | M. Orkisz An Estimate of the Influence of the Compressor Stability Margin on the Pick-Up Time of a Turbojet Engine Engineering Transactions |
| title | An Estimate of the Influence of the Compressor Stability Margin on the Pick-Up Time of a Turbojet Engine |
| title_full | An Estimate of the Influence of the Compressor Stability Margin on the Pick-Up Time of a Turbojet Engine |
| title_fullStr | An Estimate of the Influence of the Compressor Stability Margin on the Pick-Up Time of a Turbojet Engine |
| title_full_unstemmed | An Estimate of the Influence of the Compressor Stability Margin on the Pick-Up Time of a Turbojet Engine |
| title_short | An Estimate of the Influence of the Compressor Stability Margin on the Pick-Up Time of a Turbojet Engine |
| title_sort | estimate of the influence of the compressor stability margin on the pick up time of a turbojet engine |
| url | https://et.ippt.pan.pl/index.php/et/article/view/1622 |
| work_keys_str_mv | AT morkisz anestimateoftheinfluenceofthecompressorstabilitymarginonthepickuptimeofaturbojetengine AT morkisz estimateoftheinfluenceofthecompressorstabilitymarginonthepickuptimeofaturbojetengine |