Numerical Investigation on Aerodynamic Vector Performance of a Axisymmetric Bypass Dual Throat Nozzle

Author:

Xia Xuefeng,Sun Zhensheng,Hu Yu,Qu Huang,Li Siye,Zhang Yin,Liu Jipeng

Publisher

Springer Nature Singapore

Reference23 articles.

1. Zhou, H.C.: Computational Study of a Vector-Enhanced Dual-Throat Thrust-Vectoring Nozzle qand Experimental Validation. Nanjing University of Aeronautics and Astronautics, Nanjing (2009)

2. Cong, R., Wu, J.Q., Zhang, C.F.: Numerical research on jet tab thrust vector nozzle aerodynamic characteristics. J. Phys. Conf. Ser. 1300(1), 012089 (2019). https://doi.org/10.1088/1742-6596/1300/1/012089

3. Li, K.X., Eriqitai, Han, J.: Studies on control method of two dimensional fluidic throat skewing vectoring nozzle. J. Propul. Technol. 33(6), 946–950 (2012)

4. Fan, Z.P., Xu, J.L., Guo, S.: Effects of secondary injection pipe on dual throat nozzle thrust-vectoring performances. J. Propul. Technol. 35(9), 1174–1180 (2014)

5. Gu, R., Xu, J.L.: Effects of cavity on the performance of dual throat nozzle during the thrust-vectoring starting transient process. J. Eng. Gas Turbine Power 136(1), 145021–145026 (2014)

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