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
Optimum Design of High Aspect Ratio Wings Subject to Aeroelastic Constraints
Flutter Analysis of Composite Wings Using an Exact Dynamic Stiffness Matrix Method