SAE AIR 5656 : 2016
Current
The latest, up-to-date edition.
STATISTICAL STABILITY ASSESSMENT
Hardcopy , PDF
English
16-03-2016
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1. SCOPE
2. REFERENCES
3. DESCRIPTION OF MONTE CARLO METHODOLOGY
4. STATISTICAL STABILITY ASSESSMENT (SSA)
5. DESCRIPTION OF SIMULATION MODELS
6. APPLICATION OF STATISTICAL STABILITY
ASSESSMENT
7. VALIDATION OF SSA
8. SYSTEM APPLICATIONS
9. EXTENSIONS TO OTHER GAS TURBINE
APPLICATIONS
10. CONCLUDING REMARKS
11. NOTES
APPENDIX A - RANDOM NUMBER GENERATORS
APPENDIX B - CURRENT PRACTICE AND LIMITATIONS
APPENDIX C - DEPENDENCY OF VARIABLES
APPENDIX D - TYPES OF STATISTICAL DISTRIBUTIONS
This SAE Aerospace Information Report (AIR) provides a methodology for performing a statistical assessment of gas-turbine-engine stability-margin usage.
| Committee |
S-16
|
| DocumentType |
Standard
|
| Pages |
73
|
| ProductNote |
This standard is stabilized now
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| SAE AIR 1419 : 2017 | INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES |
| SAE AIR 5686 : 2010 | A METHODOLOGY FOR ASSESSING INLET SWIRL DISTORTION |
| SAE AIR 5866 : 2008 | AN ASSESSMENT OF PLANAR WAVES |
| SAE AIR 1419 : 2013 | INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES |
| SAE ARP 210 : 2014 | DEFINITION OF COMMONLY USED DAY TYPES (ATMOSPHERIC AMBIENT TEMPERATURE CHARACTERISTICS VERSUS PRESSURE ALTITUDE) |
| SAE ARP 1420 : 2002 | GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES |
| MIL-HDBK-310 Base Document:1997 | DEPARTMENT OF DEFENSE HANDBOOK - GLOBAL CLIMATIC DATA FOR DEVELOPING MILITARY PRODUCTS |
| SAE AS681K | GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS |
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