AIR1419B Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines

Revised

05/28/2013

Features
Issuing Committee
Scope
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.
Rationale
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/AIR1419B
Pages
223
Citation
SAE International Information Report, Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines, SAE Standard AIR1419B, Revised May 2013, Reaffirmed July 2011, Issued May 1983, https://doi.org/10.4271/AIR1419B.
Additional Details
Publisher
Published
May 28, 2013
Product Code
AIR1419B
Content Type
Information Report
Status
Revised
Language
English

Revisions