Parametric Aerodynamic Study of a Convertible Aircraft Using CFD Tools. ProVANT EMERGENTIa Project
Dynamic Inversion-Based Flight Control for Supersonic Civil Aircraft with High Angle of Attack
Efficient Design of Airfoil Employing XFLR for Smooth Aerodynamics of Drone
AOA and AOS Estimation of Low-Cost Light and Small UAV with Simple Sensor Configuration
Angle-of-Attack Protection Control Law Design Based on Phase Plane Analysis
Design and Aerodynamic Enhancement of Wing for BMW 5 Series Model
Design of Aircraft Angle of Attack Control Law Based on Model-Free Adaptive Control
Experimental Analysis of Implementing Roughness on NACA 0018 Airfoil
Aerodynamic Test Study on Slender Air Vehicle at Extra-Wide Angle-of-Attack
Maximum Landing Footprint Calculation Method with Angle of Attack Optimization for Reentry Vehicle
Influence of Continuous Jet at the Lower Surface on Airfoil Aerodynamic Performance
Research on a Rolling Missile Analysis Method Based on the Angle of Attack
Trajectory Optimization and Control Algorithm of Perch Landing for Fixed-Wing Aircraft
Experimental Study on Low-Speed Wing Rock Characteristics of Low Aspect Ratio Flying Wing
A Three-Dimensional Guidance Law for Cooperative Attack of Multi-UAVs
Thin Foil Theory – Lifting Flow Properties
Aerodynamics Characteristics of Compound Delta Wing at High Altitude
SC Motion Affected by an Aerodynamic Torque