Aeroelastic optimization of high aspect ratio wings using an exact dynamic stiffness matrix method
Aeroelastic Optimization of High Aspect Ratio Wings Using an Exact Dynamic Stiffness Matrix Method
Research and Development on the Parameterized Aeroengine Structural Scheme Design System
The Design of Inertia Platform with Reverse Frame Normalizing Theory
The Decoupling Design of Aircraft Lateral Flight Control Systems with Eigenstructure Assignment
Optimum Design of High Aspect Ratio Wings Subject to Aeroelastic Constraints
Flutter Analysis of Composite Wings Using an Exact Dynamic Stiffness Matrix Method
Study of the electro-optic polymer films with improved properties
Detecting multicolored object in image by content [3545-105]
New threshold method based on morphology and fourth central moment [3545-81]
Liquid thermal diffusivity measurement by pulsed photothermal deflection technique [3550-42]
Stability and optical properties of DMACB/PEK-c polymer films [3556-09]
Structural, dielectric, and optical properties of PT/PEK-c electro-optic polymer films [3556-16]
Self-Q-switched double-cladding fiber laser based on SBS [4225-39]
Self-Q-switched Er-doped fiber laser [4225-38]
A Ferroelectric Frequency-Doubling Material-Potassium Lithium Niobate
Comparisons of three methods of PN code acquisition under large Doppler shift [5253-41]
Fatigue Characteristics of Modified Asphalts and SMA
Aeroelastic Effect on Flapping Wing Performance AIAA Paper 2007-2412 CD-ROM Number 7
Fuzzy Logic-Based Urban Traffic Congestion Evaluation Models and Applications
A New Method for Solving Routing and Wavelength Assignment Problems in Optical Networks
Potential-Flow-Based Aerodynamic Analysis of a Flapping Wing
Effects of low pressure and hypoxia on growth and development of wheat
Design, Analysis and Testing of Composite Sandwich T-Joint Structures
Optimal Design of a Seamless Aeroelastic Wing Structure
Rolling Active Control for an Aircraft of Seamless Aeroelastic Wing
Optimal design of an aeroelastic wing structure with seamless control surfaces
A Composite Wing Structure with a Morphing Leading Edge
Design and Analysis of a Morphing Flap Structure for High Lift Wing
A Flexible Wing with Conformal Control Surfaces for Optimum Trim of a Tailless Air Vehicle
Structural and Dynamic Analysis of a Seamless Aeroelastic Wing
Design Improvement and Experiment of a Sandwich T-Joint Structure
SEPARATION CONTROL USING DBD PLASMA ACTUATORS: THRUST ENHANCEMENT STUDIES
Control of an Aeroelastic System with Control Surface Nonlinearity
Detached-Eddy Simulation of Cavity Flame-holding in Supersonic
Design, Experiment and Aerodynamic Calculation of a Flapping Wing Rotor Micro Aerial Vehicle