SAE AIR1419C PDF | Request Standard
Historical

SAE AIR1419C

Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines

Standard by SAE International, 2017-11-20

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Language: English

License Type: Single User

Updates: Not Included

SAE AIR1419C

AIR1419C.pdf

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.
SKU: 5846c3951fc9

  • 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
  • New Version Available: AIR1419D (2023-08-01)
  • This Version: AIR1419C (2017-11-20)
  • Previous Version: AIR1419B (2013-05-28)
  • Previous Version: AIR1419A (2011-07-19)
  • Previous Version: AIR1419 (1983-05-01)

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