Formulation of a helicopter rotor system damage detection methodology

Journal of the American Helicopter Society

Volumn 41, Issue 4, 1996, Pages 302-312

  Ganguli, Ranjan ^a   Chopra, Inderjit ^a   Haas, David J ^b  

^a UNIVERSITY OF MARYLAND   (United States)

^b NAVAL SURFACE WARFARE CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEMS; DAMPING; FAILURE ANALYSIS; FINITE ELEMENT METHOD; FLIGHT DYNAMICS; MATHEMATICAL MODELS; MOISTURE; STIFFNESS; TURBOMACHINE BLADES; VIBRATIONS (MECHANICAL);

BLADE TIP RESPONSE; DAMAGE DETECTION; FORWARD FLIGHT; LAG DAMPER; MASS; MOISTURE ABSORPTION; PITCH CONTROL SYSTEM; PITCH LINK; TRAILING EDGE FLAP; VIBRATORY HUB MOMENTS;

HELICOPTER ROTORS;

EID: 0030257668     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/jahs.41.302     Document Type: Article

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