AIR1419C Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines
Revised
11/20/2017
- Features
- Issuing Committee
- Content
- 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.
- Content
- 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.
- Pages
- 226
- Citation
- SAE International Information Report, Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines, SAE Standard AIR1419C, Revised November 2017, Reaffirmed July 2011, Issued May 1983, https://doi.org/10.4271/AIR1419C.