| Alternative title | Estimation de la course de fonctionnement d'une turbine à gaz J85-CAN-15 |
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| Download | - View final version: Gas turbine engine operating line estimation for the J85-CAN-15 engine (PDF, 5.1 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003526 |
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| Author | Search for: Bird, J. W.1; Search for: MacLeod, J.1 |
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| Affiliation | - National Research Council of Canada. Division of Mechanical Engineering
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| Format | Text, Technical Report |
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| Physical description | 33 p. |
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| Abstract | Aerothermodynamic modelling of gas turbine engines without the use of manufacturer's design data requires specialized analysis. Test cell data and empirical relationships are used to develop reasonable estimates, which are thermodynamically consistent. The specific application presented in this report is for the J85 engine with afterburner. Both design point and operating line estimation methods are presented in the form of algorithms. Methodologies for temperature-limited and afterburner operation are also provided. |
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| Publication date | 1988-08 |
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| Publisher | National Research Council Canada |
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| Series | |
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| Language | English |
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| Peer reviewed | No |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | 32fbd827-7a55-4895-a3f1-6d30ab4eff0b |
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| Record created | 2025-07-09 |
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| Record modified | 2025-11-03 |
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