Proceedings of the 2nd International Conference on Mechatronics Engineering and Information Technology (ICMEIT 2017)

Emission Properties and Stability of Internal Air Launch System

Authors
Jie Shu, Dengcheng Zhang, Lin Li, Ang Qin, Binlin Ma, Shuguang Li
Corresponding Author
Jie Shu
Available Online May 2017.
DOI
https://doi.org/10.2991/icmeit-17.2017.34How to use a DOI?
Keywords
internal air launch system, emission performance index, generalized stability, stability domain.
Abstract
Aiming at the characteristics of complex structure, changeable movement and the difference in emission and stability, put forward the emission performance index based on the study of internal air launch system; study the influence of the initial pitch angle of the carrier, characteristic diameter of stabilization parachute and some other characteristic parameters on emission properties; study the system's stability and put forward the concept of generalized stability through the research of kinetic equation, moreover, calculate stability domain through Monte Carlo calculation method.
Open Access
This is an open access article distributed under the CC BY-NC license.

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Cite this article

TY  - CONF
AU  - Jie Shu
AU  - Dengcheng Zhang
AU  - Lin Li
AU  - Ang Qin
AU  - Binlin Ma
AU  - Shuguang Li
PY  - 2017/05
DA  - 2017/05
TI  - Emission Properties and Stability of Internal Air Launch System
BT  - Proceedings of the 2nd International Conference on Mechatronics Engineering and Information Technology (ICMEIT 2017)
PB  - Atlantis Press
SP  - 187
EP  - 192
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmeit-17.2017.34
DO  - https://doi.org/10.2991/icmeit-17.2017.34
ID  - Shu2017/05
ER  -