1. Cao, Y.F.: Jet thrust vector control. Nanjing University of Aeronautics and Astronautics, Nanjing China, Master (2011)
2. Yang, F., Li, Z.H., Li, J.C.: Research progress on nozzle profile of solid rocket motor. Vacuum 57(1), 40–47 (2020)
3. Chen, Y.L., Yu, K.K., X, J.L.: Design of thrust nozzle for scramjet with geometric dimension constraint. Acta Aeronaut. Astronaut. Sin. 42(6), 124259 (2021)
4. Zhou, H.C., Han, H.J., Li, X.P.: A design method of complex variable section inlet. J. Aerosp. Power 24(6), 1357–1363 (2009)
5. Wu, S.H., Liao, D.X., Chen, J.M., et al.: Optimization design of supersonic nozzle profile based on spline curve description. J. Northwest. Polytech. Univ. 036(004), 785–791 (2018)