Parametric Aerodynamic Study of a Convertible Aircraft Using CFD Tools. ProVANT EMERGENTIa Project
Efficient Design of Airfoil Employing XFLR for Smooth Aerodynamics of Drone
Dynamic Inversion-Based Flight Control for Supersonic Civil Aircraft with High Angle of Attack
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
Experimental Analysis of Implementing Roughness on NACA 0018 Airfoil
Design of Aircraft Angle of Attack Control Law Based on Model-Free Adaptive Control
Design and Aerodynamic Enhancement of Wing for BMW 5 Series Model
Maximum Landing Footprint Calculation Method with Angle of Attack Optimization for Reentry Vehicle
Research on a Rolling Missile Analysis Method Based on the Angle of Attack
Influence of Continuous Jet at the Lower Surface on Airfoil Aerodynamic Performance
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
Thin Foil Theory – Lifting Flow Properties
A Three-Dimensional Guidance Law for Cooperative Attack of Multi-UAVs