SAE AIR 5656A:2016-03-16

This SAE Aerospace Information Report (AIR) provides a methodology for performing a statistical assessment of gas-turbine-engine stability-margin usage. Consideration is given to vehicle usage, fleet size, and environment to provide insight into the probability of encountering an in-service engine stall event. Current industry practices, such as ARP1420, supplemented by AIR1419, and engine thermodynamic models, are used to determine and quantify the contribution of individual stability threats. The statistical technique adopted by the S-16 committee for performing a statistical stability assessment is the Monte Carlo method (see Applicable References 1 and 2). While other techniques may be suitable, their application is beyond the scope of this document. The intent of the document is to present a methodology and process to construct a statistical-stability-assessment model for use on a specific system and its mission or application.

Author	SAE
Editor	SAE
Document type	Standard
Format	File
ICS	49.020 : Aircraft and space vehicles in
Number of pages	73
Replace	SAE AIR 5656:2008-03-04
Set	AEROPAKS10U-10
Year	2016
Document history	SAE AIR 5656:2008-03-04
Country	USA
Keyword	SAE 5656;SAE AIR5656A;SAE AIR5656A;SAE AIR 5656