Proceedings of the 2nd International Conference on Computer Engineering, Information Science & Application Technology (ICCIA 2017)

Numerical Simulation of Pintle Thrust Adjustable Solid Rocket Motor

Authors
Guancheng Pan, Xiong Chen, Xiaobing Ye
Corresponding Author
Guancheng Pan
Available Online July 2016.
DOI
https://doi.org/10.2991/iccia-17.2017.7How to use a DOI?
Keywords
Thrust adjustable, solid rocket motor, Nozzle efficiency.
Abstract
Numerical simulation of the flow field inside pintle controlled solid rocket motor was performed. The effects to nozzle performance with different pintle contour shapes and pintle position were investigated. The results showed that the influence of these factors to pintle nozzle efficiency was evident. The conclusion would be helpful for design experiment and application of pintle controlled solid rocket motor.
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This is an open access article distributed under the CC BY-NC license.

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Proceedings
2nd International Conference on Computer Engineering, Information Science & Application Technology (ICCIA 2017)
Part of series
Advances in Computer Science Research
Publication Date
July 2016
ISBN
978-94-6252-361-6
ISSN
2352-538X
DOI
https://doi.org/10.2991/iccia-17.2017.7How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

TY  - CONF
AU  - Guancheng Pan
AU  - Xiong Chen
AU  - Xiaobing Ye
PY  - 2016/07
DA  - 2016/07
TI  - Numerical Simulation of Pintle Thrust Adjustable Solid Rocket Motor
BT  - 2nd International Conference on Computer Engineering, Information Science & Application Technology (ICCIA 2017)
PB  - Atlantis Press
SP  - 43
EP  - 49
SN  - 2352-538X
UR  - https://doi.org/10.2991/iccia-17.2017.7
DO  - https://doi.org/10.2991/iccia-17.2017.7
ID  - Pan2016/07
ER  -