Analysis and Development of a Total Energy Control System for a Large Transport Aircraft
Interaction of a Conical Shock Wave with a Turbulent Boundary Layer
New Model of Bird Impact Analysis and Its Engineering Solution
Development of a System for Aerodynamic Fast-Response Probe Measurements
Parameter Estimation Techniques for Flight Flutter Test Analysis
Adaptive Intermittent Maneuvers of Passive Homing Missiles for Intercept Performance Improvement
Contrasting Factors in the Design Specification and Verification of Aircraft and Spacecraft Systems
The Fretting Damage and Effect of Temperature in Typical Joint of Aircraft Construction
Integration of Flight Control and Carrier Landing Aid System
Aerodynamic Characteristics of Transport Airplanes in Low Speed Configuration
Aeroelastic Analysis of Composite Wing with Control Surface
On an Extension of the Kutta-Joukowski Theorem to the Supersonic Regime
Parametric Aeroelastic Analysis of Composite Wing-Boxes with Active Strain-Energy Tuning
An Experimental Study for Interaction Flow Between Shock Wave and Turbulent Boundary Layer
The Ways of the Formation of the Horseshoe Vortex in Turbulent Boundary Layers
Structural Optimization in Preliminary Aircraft Design: a Finite-Element Approach
Aeroelastic Stability Characteristics of Composite Cylindrical Shells by the Finite Element Method
Main Landing Gear Plastic Limit Analysis for Fighter Aircraft
Assessment and Correction of Tunnel Wall Interference by Navier-Stokes Solutions
A Prediction Method of the Stalling for Wings with Rear Separation
An Approach to Prediction for Naturally Short Fatigue Crack Growth Behaviours
A New Dynamic Performance Improvement Method for Multi-Sensor Systems
Feasibility Study for an Active Aeroelastic Control System for the F-16 Aircraft