Statistical Stability Assessment
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Product Code: AIR5656
Date Published: 2008-03-04
Issuing Committee:
S-16 Turbine Engine Inlet Flow Distortion Committee
Scope
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.
Product Status: In Stock
File Size:
1108K
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| Current & Historical versions of this standard |
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| Standard |
Date published |
?Status |
| AIR5656 |
2008-03-04 |
Issued |
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