SAE AIR 1419C:2017-11-20

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.

Author	SAE
Editor	SAE
Document type	Standard
Format	File
ICS	49.050 : Aerospace engines and propulsion systems
Number of pages	226
Replace	SAE AIR 1419B:2013-05-28
Set	AEROPAKS10U-10
Year	2017
Document history	SAE AIR 1419B:2013-05-28
Country	USA
Keyword	SAE 1419;SAE AIR1419C;SAE AIR1419C;SAE AIR 1419