A STUDY OF PLANE FLOWS USING MICROCOMPUTERS

Numerical Solution of Inviscid Transonic Flow Using Hybrid Finite Volume-Finite Difference Solution Technique on Unstructured Grid

MICROCOMPUTER GRID GENERATION FOR TWO-DIMENSIONAL AERODYNAMIC APPLICATIONS

Computational Techniques for Calculation of Missile Aerodynamic Coefficients

Computational Techniques for Calculation of Missile Aerodynamic Coefficients

Computing Lower Critical Mach Number by a Simple Method

IMPLICIT TIME-DEPENDENT METHOD FOR THE CALCULATION OF TRANSONIC BLADE-TO-BLADE FLOWS WITH STRONG SHOCK WAVES

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

NUMERICAL SOLUTION OF INVISCID FLOW AROUND 3D AERIAL VEHICLES

ON THE CALCULATION OF LAMINAR BOUNDARY-LAYER FLOWS WITH MASS TRANSFER BY A SIMPLE INTEGRAL METHOD