An experimental-theoretical correlation study of non-linear bending and torsion deformations of a cantilever beam

Journal of Sound and Vibration

Volumn 50, Issue 4, 1977, Pages 533-544

  Dowell, E H ^a   Traybar, J ^a   Hodges, D H ^b  

^a PRINCETON UNIVERSITY   (United States)

^b Army Air Mobility Research and Development Laboratory ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

STRUCTURAL ANALYSIS - MATHEMATICAL MODELS;

BEAMS AND GIRDERS;

EID: 0017452683     PISSN: 0022460X     EISSN: 10958568     Source Type: Journal    
DOI: 10.1016/0022-460X(77)90501-6     Document Type: Article

References (7)

1. Non-linear equations of motion for the elastic bending and torsion of twisted non-uniform rotor blades
2. An experimental study of the non-linear stiffness of a rotor blade undergoing flap, lag and twist deformations
3. Aerodynamics
4. Steady flight differential equations of motion for a flexible helicopter blade with chordwise mass unbalance
5. Dynamic non-linear elastic stability of helicopter rotor blades in hover and in forward flight
6. Stability of elastic bending and torsion of uniform cantilevered rotor blades in hover
7. Stability of elastic bending and torsion of uniform cantilevered rotor blades in hover with variable structural coupling