An Estimate of the Influence of the Compressor Stability Margin on the Thrust of a Turbojet Engine
The relations derived in the paper make it possible to analyze. the influence of the compressor stability margin upon the thrust of a turbo jet engine. The engines operating within the economy range (minimum fuel consumption) and optimum range (maximum thrust) are considered.
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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/1623 |
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