SAE AIR1419B
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines
Hardcopy , PDF
26-11-2017
English
28-05-2013
Important note : Users cannot be edited or removed once added to your Multi user PDF.| DocumentType |
Standard
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| Pages |
223
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
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.
| SAE AIR 4869 : 2015 | DESIGN CONSIDERATIONS FOR ENCLOSED TURBOFAN/TURBOJET ENGINE TEST CELLS |
| SAE ARP1420C | Gas Turbine Engine Inlet Flow Distortion Guidelines |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| SAE AIR5867 | Assessment of the Inlet/Engine Total Temperature Distortion Problem |
| SAE AIR5687A | Inlet/Engine Compatibility - From Model to Full Scale Development |
| SAE AS755E | Aircraft Propulsion System Performance Station Designation and Nomenclature |
| SAE AIR5656A | Statistical Stability Assessment |
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