|Table of Contents|

Influence of throat curvature radius on characteristic of maximum thrust nozzle(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2010年05期
Page:
36-39
Research Field:
研究与设计
Publishing date:

Info

Title:
Influence of throat curvature radius on characteristic of maximum thrust nozzle
Author(s):
CHI Bao-hua;  HONG Liu;  LI Long-fei;  YANG Guo-hua;  XU Yun-fei
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
-
PACS:
V434
DOI:
-
Abstract:
The contours of a maximum thrust nozzle are designed and calculated for different throat structures. The influence of throat curvature radius on flow coefficient, geometry efficiency, thrust coefficient, divergence loss and location of flow separation point is analyzed. The results show that the flow coefficient increases with the increase of the upstream curvature radius, the thrust coefficient and geometry efficiency decrease with the increase of the downstream curvature radius, the divergence loss decreases with the increase of downstream curvature radius in a small

References:

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