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Black Hawk helicopter vibration analysis due to main rotor damage : directional constituents of the resultant vibrations /

Black Hawk helicopter cockpit vibrations due to main rotor damage are presented based upon an analysis and computer code originally developed in-house in the Air Systems Branch (ASB) of the U.S. Army Research Laboratory (ARL). Ballistic damage is simulated by removing various amounts of the outer ra...

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Bibliographic Details
Main Author: Fries, Joseph C.
Corporate Author: U.S. Army Research Laboratory
Format: Government Document eBook
Language:English
Published: Aberdeen Proving Ground, MD : U.S. Army Research Laboratory, [2001]
Series:ARL-TR (Aberdeen Proving Ground, Md.) ; 2442.
Subjects:
Black Hawk (Military transport helicopter)
Vibration (Aeronautics) > Physiological effect.
Rotors (Helicopters)
Helicopters.
Flight testing.
Vibration.
Helicopter rotors.
Experimental data.
Aircraft maintenance.
Cockpits.
Damage assessment.
Attrition.
Rotor blades(rotary wings)
Aircraft equipment.
Transport aircraft.
Fatigue tests(mechanics)
VIBRATION ANALYSIS
BLACK HAWK HELICOPTER
Online Access:https://purl.fdlp.gov/GPO/gpo3356

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https://purl.fdlp.gov/GPO/gpo3356

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Call Number: D 101.133:2442
 
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D 101.133:2442 Available