Abstract
A study of an incompressible two-dimensional flow in a channel with one porous wall is presented in this research. As usual, the cylindrical propellant grain of a solid rocket motor is modeled as a long tube with one end closed at the headwall, while the other remains open. The governing continuity and momentum equations together with the associated boundary conditions are first reduced to a set of self similar non-linear coupled ordinary differential equations using similarity transformations. Then we solved the ordinary differential equation by RVIM and the numerical method.
Original language | English |
---|---|
Pages (from-to) | 379-387 |
Number of pages | 9 |
Journal | Mechanics and Mechanical Engineering |
Volume | 21 |
Issue number | 2 |
Publication status | Published - 2017 |
Externally published | Yes |
Keywords*
- Analytical approach
- DTM
- Flow modeling
- Porous cylinder
- Solid rocket motors
Field of Science*
- 2.5 Materials engineering
- 1.3 Physical sciences
- 2.3 Mechanical engineering
Publication Type*
- 1.1. Scientific article indexed in Web of Science and/or Scopus database