SAE AIR 1935 : 2007
SAE AIR 1935 : 2007
METHODS OF CONTROLLING DISTORTION OF INLET AIRFLOW DURING STATIC ACOUSTICAL TEST OF TURBOFAN ENGINES AND FAN RINGS
SAE International
Abstract
Describes technical details on devices that 'condition' the airflow entering the engine to more nearly simulate flight operations without introducing a detrimental impact on sound propagating from the engine.
General Product Information
| Document Type | Standard |
| Status | Current |
| Publisher | SAE International |
| Committee | A-21 |
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SAE J 2662 : 2017
$78.00 (-58%) $32.76