SAE AIR 5826 : 2017
Current
The latest, up-to-date edition.
DISTORTION SYNTHESIS/ESTIMATION TECHNIQUES
Hardcopy , PDF
English
21-03-2017
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1 SCOPE
2 REFERENCES
3 BACKGROUND
4 REVIEW OF CURRENT STATUS
5 RECOMMENDATIONS
6 NOTES
Gives a review of published methods that have been used to provide estimates of the levels of distortion and/or the concomitant loss of stability pressure ratio that can occur when the recommended full complement of aerodynamic interface plane high-response instrumentation is not used when obtaining inlet data.
| Committee |
S-16
|
| DocumentType |
Standard
|
| Pages |
15
|
| ProductNote |
This version is now stabilized.
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| SAE AIR 1419 : 2017 | INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES |
| SAE ARP 1420 : 2002 | GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES |
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