Zhao Jingyun. EFFECT OF GEOMETRIC PARAMETERS ON INTERNAL PERFORMANCE OF CONVERGENT-DIVERGENT NOZZLE[J]. Journal of Aerospace Power, 1989, 4(3): 273-274,295.
Citation:
Zhao Jingyun. EFFECT OF GEOMETRIC PARAMETERS ON INTERNAL PERFORMANCE OF CONVERGENT-DIVERGENT NOZZLE[J]. Journal of Aerospace Power, 1989, 4(3): 273-274,295.
Zhao Jingyun. EFFECT OF GEOMETRIC PARAMETERS ON INTERNAL PERFORMANCE OF CONVERGENT-DIVERGENT NOZZLE[J]. Journal of Aerospace Power, 1989, 4(3): 273-274,295.
Citation:
Zhao Jingyun. EFFECT OF GEOMETRIC PARAMETERS ON INTERNAL PERFORMANCE OF CONVERGENT-DIVERGENT NOZZLE[J]. Journal of Aerospace Power, 1989, 4(3): 273-274,295.
The efect of geometric parameters on internal performance of convergent-divergent nozzle has been investigated experimentally. The relationships of thrust coefficient and wall static pressure distribution to area ratio, divergent angle, convergent angle and throat radius of curvature are presented in this paper.