SAE AIR5867
Current
The latest, up-to-date edition.
Assessment of the Inlet/Engine Total Temperature Distortion Problem
Hardcopy , PDF
English
21-11-2017
RATIONALE
1 SCOPE
2 REFERENCES
3 CONCLUSIONS
4 INLET TOTAL TEMPERATURE DISTORTION
PROBLEM ASSESSMENT
5 STATUS OF PAST AND PRESENT EFFORTS
6 SUGGESTED APPROACH TO A TOTAL
TEMPERATURE DISTORTION METHODOLOGY
APPENDIX A - PROPOSED SPATIAL TOTAL
TEMPERATURE DISTORTION DESCRIPTORS
APPENDIX B - TOTAL TEMPERATURE
RAMP/DISTORTION METHODOLOGY
APPENDIX C - SIMILARITY AND SCALING
REQUIREMENTS
This report revises ARD50015 document to the AIR format.
DevelopmentNote |
Supersedes & Redesignates SAE ARD 50015. (11/2017)
|
DocumentType |
Standard
|
Pages |
57
|
PublisherName |
SAE International
|
Status |
Current
|
This report revises ARD50015 document to the AIR format. This report, as was the original, is intended to complement ARP1420C and AIR1419C documents issued by the SAE S-16 Committee on spatial total-pressure distortion. These previous documents addressed only total-pressure distortion and excluded total temperature distortion.The subject of inlet total temperature distortion is addressed in this report with some background and identification of the problem area. The status of past efforts is reviewed, and an attempt is made to define where we are today. Deficiencies, voids, and limitations in knowledge and test techniques for total temperature distortion are identified.
SAE AIR1419B | Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines |
MIL-E-5007 Revision D:1973 | ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR |
SAE ARP 1420 : 2002 | GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES |
SAE ARP246D | Orientation of Engine Axis, Coordinate and Numbering Systems for Aircraft Gas Turbine Engines |
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