SAE AIR1419C
Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines
Historical
Standard by SAE International, 2017-11-20
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About This Item
This document addresses many of the significant issues associated with effects of inlet total-pressure distortion on turbine-engine performance and stability. It provides a review of the development of techniques used to assess engine stability margins in the presence of inlet total-pressure distortion. Specific performance and stability issues that are covered by this document include total-pressure recovery and turbulence effects and steady and dynamic inlet total-pressure distortion.
The intent of this document is to provide a basic understanding of the effects of inlet total-pressure distortion on the performance of gas turbine engines, particularly in military applications. The document was revised to incorporate an Introduction containing material inadvertently omitted from revision B.
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Standard Details
- Publication Date: 2017-11-20
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Standard
- Subject: Engine control systems, Auxiliary power units, Computational fluid dynamics, Engine components, Finite element analysis, Wind tunnel tests, Gas turbines, Environmental testing, Hypersonic and supersonic aircraft
- Official SAE: Doi link
