Computational Techniques for Calculation of Missile Aerodynamic Coefficients

Computational Techniques for Calculation of Missile Aerodynamic Coefficients

Development of a Comprehensive Tool for Calculating the Aeromechanics Characteristics of High-Speed Aircraft

AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES

Surrogate Representation for the Aerodynamic Coefficients of Supersonic Airfoils

Preliminary Investigation on the Impact of Missile Design on its Aerodynamic Features

NUMERICAL SOLUTION OF INVISCID FLOW AROUND 3D AERIAL VEHICLES

CALCULATION OF AERODYNAMIC HEATING OF A CONICAL FOREBODY ALONG FLIGHT TRAJECTORY

APPLICATION OF GENETIC ALGORITHMS WITH THE AID OF PANEL METHOD TO OPTIMIZE MISSILE AERODYNAMIC SHAPE

Computational Solution of Aircraft Stability Derivatives