Development and verification of AeroMech tool for rapid estimation of airplane aerodynamic characteristics during early design stages

Computational Aerodynamics Analysis of a Light Aircraft

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

Calculating Aerodynamic & Stability Characteristics For Small fixed-wing UAVs based on Digital DATCOM

Aerodynamic/Structural Optimization of a Training Aircraft Wing

Computational Techniques for Calculation of Missile Aerodynamic Coefficients

Computational Techniques for Calculation of Missile Aerodynamic Coefficients

Calculating Aerodynamic & Stability Characteristics for a MALE UAV using USAF Digital DATCOM

AERODYNAMIC PERFORMANCE AND ASSOCIATED NOISE GENERATION SPECTRA OF AIRFOIL

DEVELOPMENT OF A COMPUTER BASED LEARNING TOOL FOR UNDERSTANDING AIRCRAFT STRUCTURES