[图书][B] Nonlinear composite beam theory

DH Hodges - 2006 - arc.aiaa.org
Description From an authoritative expert whose work on modern helicopter rotor blade
analysis has spanned over three decades, comes the first consistent and rigorous …

On the modeling of integrally actuated helicopter blades

CES Cesnik, S Shin - International Journal of Solids and Structures, 2001 - Elsevier
This paper presents an asymptotical formulation for preliminary design of multi-cell
composite helicopter rotor blades with integral anisotropic active plies. It represents the first …

[HTML][HTML] Design and aeroelastic analysis of active twist rotor blades incorporating single crystal macro fiber composite actuators

JS Park, JH Kim - Composites Part B: Engineering, 2008 - Elsevier
The advanced active twist rotor (AATR) blade incorporating single crystal macro fiber
composite (single crystal MFC) actuators is designed and the aeroelastic analysis is …

On the twist performance of a multiple-cell active helicopter blade

CES Cesnik, SJ Shin - Smart Materials and Structures, 2001 - iopscience.iop.org
This paper discusses how torsional stiffness is related with twist actuation in an integrally
twist actuated rotor blade. It shows that increase in torsional stiffness does not necessarily …

Structural behavior of thin-and thick-walled composite blades with multicell sections

SN Jung, IJ Park - AIAA journal, 2005 - arc.aiaa.org
COMPOSITE rotor blades are, in general, builtup structures made of different materials for
the skin and spar, normally of closed single-or multicelled cross-sections, and thin walled …

Optimum coupling in thin-walled, closed-section composite beams

WK Lentz, EA Armanios - Journal of Aerospace Engineering, 1998 - ascelibrary.org
A gradient-based optimization scheme has been developed for obtaining the maximum
coupling in thin-walled composite beams subject to hygrothermal and frequency constraints …

Design, manufacturing, and testing of an active twist rotor

SJ Shin - 1999 - dspace.mit.edu
An Active Twist Rotor (ATR) is developed for future implementation of the individual blade
control for vibration and noise reduction in helicopters. The rotor blade is integrally twisted …

[PDF][PDF] Analysis of composite wing structures with a morphing leading edge

R Morishima - 2011 - researchgate.net
One of the main challenges for the civil aviation industry is the reduction of its environmental
impact. Over the past years, improvements in performance efficiency have been achieved by …

Structural analysis for designing rotor blades with integral actuators

C Cesnik, S Shin - 39th AIAA/ASME/ASCE/AHS/ASC Structures …, 1998 - arc.aiaa.org
This paper presents an asymptotical formulation for analyzing multi-cell composite
helicopter rotor blades with integral anisotropic active plies. It represents the first attempt in …

A simple mixed-based approach for thin-walled composite blades with two-cell sections

NJ Sung, P Il-Ju - Journal of mechanical science and technology, 2005 - Springer
In this work, a mixed beam approach that combines both the stiffness and the flexibility
methods has been performed to analyze the coupled composite blades with closed, two-cell …