COMPUTATIONAL MODELLING OF NON-STATIONARY PROCESSES OF THE INTERNAL SUPERSONIC GAS FLOW ON THE EXAMPLE OF THE EXIT OF THE ROCKET FROM THE STARTING CONTAINER

Authors

  • R. A. Peshkov Author
  • R. V. Sidel'nikov Author
  • V. G. Degtyar' Author

Abstract

Methods of calculations was developed. This method include non-stationary
processes of internal supersonic gas flow on an example of an exit of the rocket
from the starting container. By means of various techniques of research it was
possible to carry out the analysis of influence of design data of the starting container
for speed of movement of the rocket not only qualitatively, but also quantitatively.
The same techniques allowed to estimate influence of an external temperature factor on parameters of an exit of the rocket from the starting container.

Author Biographies

  • R. A. Peshkov
    Post-graduate student of ?Aircrafts and Automatic Installations? department
  • R. V. Sidel'nikov

    The candidate of engineering science, assistant professor of ?Aircrafts and Automatic Installations? department

  • V. G. Degtyar'

    The doctor of engineering science, professor, the Head of ?Aircrafts and Automatic Installations? department

Issue

No. 33 (2012)

Section

Calculation and design