An active-passive hybrid method for optimization of rotor blades with trailing edge flaps-Reference-Cited by-同舟云学术

An active-passive hybrid method for optimization of rotor blades with trailing edge flaps

Published:1999-04-12 Issue: Volume: Page:
ISSN:
Container-title:40th Structures, Structural Dynamics, and Materials Conference and Exhibit
language:
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Author:

Zhang Jianhua¹,Smith Edward¹,Wang K.¹

Affiliation:

1. Pennsylvania State Univ., University Park

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1222

Reference27 articles.

1. Lim, J. W. "Aeroelastic Optimization of A Helicopter Rotor," Ph.D. Thesis,University of Maryland, College Park, 1988

2. Ganguli, R. "Aeroelastic Optimization of Advanced Geometry and Composite Helicopter Rotors," Ph.D. Thesis,University of Maryland, College Park, 1994.

3. G. N. Vandeplaats. "CONMIN - A Fortran Program for Constrained Function Minimization," User's Manual, NASA TMX 62282,1973.

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1. Vibration Analysis of A Helicopter Blade with A Piezoelectric Actuated Trailing Edge Flap;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23

2. Active Load Control of an Articulated Composite Rotor Blade via Dual Trailing Edge Flaps;44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2003-04-07

3. Active Vibration Control in Rotorcraft Systems Using Smart Actuators;43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2002-04-22