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 Flexible Wing with Conformal Control Surfaces for Optimum Trim of a Tailless Air Vehicle
Analysis on Vertical Scattering Signatures in Forestry with PolInSAR
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
Detecting multicolored object in image by content [3545-105]
Effects of low pressure and hypoxia on growth and development of wheat
Electron Beam Welding of Dissimilar Materials and Image Acquisition
Fatigue Characteristics of Modified Asphalts and SMA