Test executed from June 6 through July 3, 2011. Objectives - Understand maneuver acoustics - Validate ground footprint acoustic codes - Incorporate maneuvers into acoustic ground footprint prediction codes Acoustic measurement of - Source noise - Steady and transient maneuvers - Approach profiles Large test crew: 23 people from 7 organizations. Acquired 410 individual data points over 10 testing days and 30.6 flight hours. All “Priority One” and “Priority Two” test conditions measured.
Maneuver Acoustic Flight Test of the Bell 430 Helicopter
NASA Fundamental Aeronautics Program 2012 Technical Conference ; 2012 ; Cleveland, OH, US
Miscellaneous
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English
Maneuver Acoustic Flight Test of the Bell 430 Helicopter
NTIS | 2012
|Maneuver Acoustic Flight Test of the Bell 430 Helicopter
NTRS | 2012
|Maneuver Acoustic Flight Test of the Bell 430 Helicopter
British Library Conference Proceedings | 2012
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