Computational Techniques for Calculation of Missile Aerodynamic Coefficients

AN ALGORITHM FOR CALCULATING THE AERODYNAMIC DERIVATIVES OF A SUPER-SONIC MISSILE

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

Surrogate Representation for the Aerodynamic Coefficients of Supersonic Airfoils

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

Computational Aerodynamics Analysis of a Light Aircraft

Calculation Of One-Dimensional Transonic Flows Using Micro-Computers

Computational Investigation of Base Drag Reduction for a Projectile at Different Flight Regimes

Computational Solution of Aircraft Stability Derivatives

An Investigation into the Performance of a Homing Guided Missile with Different Aerodynamic Configurations