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
An orthogonality sensitivity method for analytical dynamic model correction using modal test data
Optimum Design of High Aspect Ratio Wings Subject to Aeroelastic Constraints
Flutter Analysis of Composite Wings Using an Exact Dynamic Stiffness Matrix Method
Supermaneuverable flight control using dynamica-inversion-based neural networks
Nonlinear inversion dynamic neurocontrol method for flight decoupling control problems
Detection and isolation of control surface effectiveness failures
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]
Nonlinear dynamic inversion control for super-maneuvering aircraft
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
Development of an improved ground-based prototype of space plant-growing facility
Development of an improved ground-based prototype of space plant-growing facility
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
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