A Composite Wing Structure with a Morphing Leading Edge
AERODYNAMIC DESIGN THEORY AND METHODOLOGY FOR AN AIRFRAME-INLET INTEGRATED FULL-WAVERIDER VEHICLE
Aeroelastic Effect on Flapping Wing Performance AIAA Paper 2007-2412 CD-ROM Number 7
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
A Ferroelectric Frequency-Doubling Material-Potassium Lithium Niobate
A Flexible Wing with Conformal Control Surfaces for Optimum Trim of a Tailless Air Vehicle
Analysis on Vertical Scattering Signatures in Forestry with PolInSAR
A New Method for Solving Routing and Wavelength Assignment Problems in Optical Networks
An Improved Spatiogram Similarity Measure for Object Tracking
An orthogonality sensitivity method for analytical dynamic model correction using modal test data
Comparisons of three methods of PN code acquisition under large Doppler shift [5253-41]
Control of an Aeroelastic System with Control Surface Nonlinearity
Design, Analysis and Testing of Composite Sandwich T-Joint Structures
Design and Analysis of a Morphing Flap Structure for High Lift Wing
Design, Experiment and Aerodynamic Calculation of a Flapping Wing Rotor Micro Aerial Vehicle
Design Improvement and Experiment of a Sandwich T-Joint Structure
Detached-Eddy Simulation of Cavity Flame-holding in Supersonic