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
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]
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