Abstract: In this paper, one-dimensional analysis of flow in a
single-stage gas gun is conducted. The compressible inviscid flow
equations are numerically solved by the second-order Roe TVD
method, by using moving boundaries. For investigation of real gas
effect the Noble-Able equation is applied. The numerical results are
compared with the experimental data to validate the numerical
scheme. The results show that with using the Noble-Able equation,
the muzzle velocity decreases.