Modeling of 3-D Flow in Supersonic Nozzle Unit with Adjustable Critical Section
| Authors: Shabanov D.S., Gostev V.A., Cherepov V.I. | Published: 26.01.2014 |
| Published in issue: #2(63)/2006 | |
| Category: Simulation of Processes | |
| Keywords: | |
A technique to calculate internal ballistic characteristics of the supersonic nozzle with the unsymmetrical input is proposed. The technique is based on the numerical Godunov-Kolgan method with application of a model that divides flow surfaces. The experimental results are compared to the calculated ones.
