Geometrically exact nonlinear analysis of pre-twisted composite rotor blades-Reference-Cited by-同舟云学术

Geometrically exact nonlinear analysis of pre-twisted composite rotor blades

Published:2018-02 Issue:2 Volume:31 Page:300-309
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

SHANG Li'na,XIA Pinqi,HODGES Dewey H.

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference28 articles.

1. Aeroelastic stability analysis of a composite rotor blade;Hong;J Am Helicopter Soc,1985

2. Hodges DH, Dowell EH. Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades. Moffett Field: Ames Research Center and U.S. Army Air Mobility R&D Laboratory; 1974. Report No.: NASA TN D-7818.

3. Aeroelastic stability of a composite blade in forward flight;Panda;Vertica,1987

4. Formulation and evaluation of an analytical model for composite box-beams;Smith;J Am Helicopter Soc,1990

5. Aeroelastic response, loads and stability of a composite rotor in forward flight;Smith;AIAA J,1993

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