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Preparation of Ion Composite Photosensitive Resin and Its Application in 3D-Printing Highly Sensitive Pressure Sensor. [PDF]

Sensors (Basel)
Guan T, Li H, Liu J, Zhang W, Wang S, Ye W, Bian B, Yi X, Wu Y, Liu Y, Du J, Shang J, Li RW.   +12 more
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Computational study of axisymmetric divergent bypass dual throat nozzle

Aerospace Science and Technology, 2019
Abstract A bypass dual throat nozzle (BDTN) is a fluidic thrust-vectoring nozzle (FTVN) that is based on the conventional dual throat nozzle (DTN). The BDTN provides high thrust vectoring (TV) efficiency with low thrust loss and does not consume additional secondary flow.
Yangsheng Wang, Jinglei Xu, Shuai Huang, Yongchen Lin, Jingjing Jiang   +4 more
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A computational study of thrust vectoring control using dual throat nozzle

Journal of Thermal Science, 2010
Dual throat nozzle (DTN) is fast becoming a popular technique for thrust vectoring. The DTN is designed with two throats, an upstream minimum and a downstream minimum at the nozzle exit, with a cavity in between the upstream throat and exit. In the present study, a computational work has been carried out to analyze the performance of a dual throat ...
Choon Sik Shin, Heuy Dong Kim, Toshiaki Setoguchi, Shigeru Matsuo   +3 more
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Design and Preliminary Analysis of the Variable Axisymmetric Divergent Bypass Dual Throat Nozzle

Journal of Fluids Engineering, 2020
Abstract Turbofan engines with afterburners usually have variable nozzle throat area, and the nozzle throat area may increase by 50–100% during afterburning. An axisymmetric divergent bypass dual throat nozzle (ADBDTN) can offer high thrust vectoring efficiency without requiring additional secondary flow in the pitch and yaw directions ...
Ruifeng Pan, Jingjing Jiang, Shuai Huang, Jinglei Xu, Yangsheng Wang   +4 more
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Numerical investigation of short takeoff and landing exhaust system using bypass dual throat nozzle

Aerospace Science and Technology, 2023
Yuqi Zhang, Jinglei Xu, Ruifeng Pan, Yao Li, Zhao Ma, Shuai Huang   +5 more
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Dynamic Experimental Investigations of a Bypass Dual Throat Nozzle

Journal of Engineering for Gas Turbines and Power, 2015
The bypass dual throat nozzle (BDTN) does not consume any secondary injection from the other part of the engine, while it can produce steady and efficient vectoring deflection similar to the conventional dual throat nozzle (DTN). A BDTN model has been designed and subjected to dynamic experimental study.
Rui Gu, Jinglei Xu
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Study of Starting Problem of Axisymmetric Divergent Dual Throat Nozzle

Journal of Engineering for Gas Turbines and Power, 2017
Compared to the conventional axisymmetric dual throat nozzle, the axisymmetric divergent dual throat nozzle (ADDTN) can offer larger thrust vector angles. However, the starting problem maybe exists in the ADDTN and results in a huge thrust loss. In this paper, the ADDTN starting problem has been studied by steady and unsteady numerical simulations. The
Yangsheng Wang, Jinglei Xu, Shuai Huang
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Numerical simulation and experiment of a bypass dual throat nozzle with tab modification

Aerospace Science and Technology
Ruifeng Pan, Jinglei Xu, Yuqi Zhang, Yao Li, Shuai Huang   +4 more
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Numerical Investigation of the Thrust Vectoring Performance of a Bypass Dual Throat Nozzle

ASME 2023 Heat Transfer Summer Conference, 2023
Abstract Aircraft propulsion systems have become progressively complex due to a recent emphasis on the maneuverability of future fighter aircraft. These systems are capable of providing additional maneuverability to the aircraft. In addition to being able to withstand the high temperatures and pressures generated by modern engines, the ...
Saadia Afridi, Tariq Amin Khan, Wei Li, S. A. Sherif   +3 more
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Experimental and numerical investigation of an axisymmetric divergent dual throat nozzle

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019
The dual throat nozzle achieves higher thrust vectoring efficiencies and lesser thrust loss than other fluidic thrust-vectoring nozzles. Separation always occurs at the bottom of the cavity with complex three-dimensional characteristics for the dual throat nozzle.
Yang-Sheng Wang, Jing-Lei Xu, Shuai Huang, Yong-Chen Lin, Jing-Jing Jiang   +4 more
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