This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
DESIGN CONSIDERATIONS FOR ENCLOSED TURBOFAN/TURBOJET ENGINE TEST CELLS
- Aerospace Standard
- AIR4869
- Issued
Sector:
Issuing Committee:
Language:
English
Scope
This SAE Aerospace Information Report (AIR) has been written for individuals associated with the ground-level testing of large and small gas turbine engines and particularly for those who might be interested in upgrading their existing or acquiring new test cell facilities.
Recommended Content
| Aerospace Standard | The Coanda/Refraction Concept for Gas Turbine Engine Test Cell Noise Suppression |
| Aerospace Standard | Turbofan and Turbojet Gas Turbine Engine Test Cell Correlation |
| Aerospace Standard | Engine Erosion Protection |
Topic
Data Sets - Support Documents
No Datasets Available
Issuing Committee
EG-1E Gas Turbine Test Facilities and Equipment
The SAE EG-1E, Gas Turbine Engine Test Facilities & Equipment committee addresses all facets of test facility design, operation, maintenance, calibration and measurement, relating to gas turbine engine testing. The group is dedicated to creating, preparing, and maintaining all relevant specifications, standards, and requirements in this field.
Reference
| Number | Title |
|---|
* Redlines comparisons are available for those standards
listed in the Revision History that contain a radio button. A
redline comparison of the current version against a revision is
accomplished by selecting the radio button next to the standard and
then selecting 'compare'. At this time, Redline versions only exist
for some AMS standards. SAE will continue to add redline versioning
with ongoing updates to SAE MOBILUS.