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 |
| Published: |
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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