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
- 2.3 Mechanical engineering
- 1.3 Physical sciences
Publication Type*
- 1.1. Scientific article indexed in Web of Science and/or Scopus database
ASJC Scopus subject areas
- General Materials Science
- Automotive Engineering
- Mechanics of Materials
- Mechanical Engineering
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