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International Journal of Aerospace Engineering
Volume 2017 (2017), Article ID 4104212, 11 pages
https://doi.org/10.1155/2017/4104212
Research Article

Reduced Actuator Set for Pressure Control and Thrust Distribution for Multinozzle Propulsion Systems

1Korea Advanced Institute of Science and Technology, Daejeon 34141, Republic of Korea
2Chungnam National University, Daejeon 34134, Republic of Korea
3Agency for Defense Development, Daejeon 34186, Republic of Korea

Correspondence should be addressed to Yeerang Lim

Received 28 November 2016; Revised 13 March 2017; Accepted 20 March 2017; Published 8 May 2017

Academic Editor: Mahmut Reyhanoglu

Copyright © 2017 Yeerang Lim et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

How to Cite this Article

Yeerang Lim, Jaecheong Lee, Hyochoong Bang, Hwanil Huh, and Hosung Lee, “Reduced Actuator Set for Pressure Control and Thrust Distribution for Multinozzle Propulsion Systems,” International Journal of Aerospace Engineering, vol. 2017, Article ID 4104212, 11 pages, 2017. doi:10.1155/2017/4104212