The model of spatial supersonic flow in the nozzle with asymmetric input
| Authors: Nikitin D.P., Gostev V.A., Poliansky A.R. | Published: 29.03.2015 |
| Published in issue: #2(35)/1999 | |
| Category: Simulation of Processes | |
| Keywords: | |
The calculation method is considered allowing to determine the pressure distribution on the wall of the supersonic nozzle with an asymmetric flap. The numerical method by Godunov-Kolgan using the model of the separating surface of the flow, form the basis for this method development. The comparative analysis of the experimental data with calculation results, is presented.
