Three Dimensional Simulation of Supersonic Flow over Missiles of Different Shapes
Three Dimensional Simulation of Supersonic Flow over Missiles of Different Shapes

Jalal M. Jalil; Hussain H. Al-Kayiem; Ahmed Kadhim Hussein

Volume 30, Issue 3 , January 2012, , Page 325-343

https://doi.org/10.30684/etj.30.3.1

Abstract
  In this work, a three-dimensional primitive variable of supersonic flow over missiles was computed based on finite difference computational fluid dynamic methods. The problem was considered ...  Read More ...
Shock Wave Capturing Numerically in Two Dimensional Supersonic Wind Tunnel for Different Configuration
Shock Wave Capturing Numerically in Two Dimensional Supersonic Wind Tunnel for Different Configuration

Ahmed Fouad Mahdi

Volume 30, Issue 3 , January 2012, , Page 426-442

https://doi.org/10.30684/etj.30.3.8

Abstract
  Numerical solutions of two dimensional Euler equations are obtained for transonic and supersonic flows. The shock capturing method is employed to solve compressible Euler equations ...  Read More ...