Abstract
To understand influence of structure parameters on heat transfer in round to rectangular nozzle (RR nozzle), several RR nozzles were designed. Three parameters were taken into consideration: round to rectangular transforming position, ratio of height to width and arc radius at exit. Three dimensional Navier-Stokes equations were solved with finite volume method. Standard k-ε turbulent model and wall function were used for near wall treatment. The coupling of pressure and velocity were realized with SIMPLE algorithm. Results indicate: under conditions that contour derivative is consecutive, transforming position does not significantly affect heat transfer in RR nozzles; height to width ratio at exit greatly influences heat transfer in RR nozzles and too small ratio would lead to high temperature points on gas side wall; arc radius has an effect on surface temperature of perimeter of gas side wall and too small radius makes circumferential temperature non-uniform.
Original language | English |
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Pages (from-to) | 489-494 |
Number of pages | 6 |
Journal | Tuijin Jishu/Journal of Propulsion Technology |
Volume | 26 |
Issue number | 6 |
Publication status | Published - Dec 2005 |
Externally published | Yes |
Keywords
- Internal nozzle
- Liquid propellant rocket engine
- Numerical simulation
- Plug nozzles
- Regenerative cooling