1. Sutton, G.P. and Biblarz, O., "Rocket Propulsion Elements", John Wiley & Sons Inc, New York, (2001).
2. Gubse, R.D. "An experimental investigation of thrust vector control by secondary injection," NASA CR-297, (1965).
3. Dhinagaran, R. and Bose, T.K. "Comparison of Euler and Navier-Stokes solutions for nozzle flows with secondary injection", AIAA Paper 96-0453, AIAA 34th Aerospace Sciences Meeting and Exhibit, Reno, NV Jan 15-18, (1996).
4. Lee, S.H., "Characteristics of dual transverse injection in scramjet combustor, Part 1: Mixing", Journal of Propulsion and Power, Vol. 22, No. 5, (2006).
5. Anantesha, S.N. and Vamsidhar, D., "Numerical investigation and parametric study of fluidic thrust vectoring by shock vector control method, " SASTECH ,Vol. 6, No. 2, (2007).
6. Shin, C.S., "A computational study of thrust vectoring control using dual throat nozzle," Journal of Thermal Science, Vol. 19, No. 6 , pp. 486-490, (2010).
7. Deng, R., Kong, F. and Kim, H.D., "Numerical simulation of fluidic thrust vectoring in an axisymmetric supersonic nozzle," Journal of Mechanical Science and Technology, Vol. 28, No. 12, pp. 4979-4987, (2014).
8. Zmijanovic, V., Lago, V., Sellam, M. and Chpoun, A., "Thrust shock vector control of an axisymmetric conical supersonic nozzle via secondary transverse gas injection," Shock Waves, Vol. 24, No. 1, pp. 97-111, (2014).
9. Deng, R., Setoguchi, T. and Kim, H.D., "Large eddy simulation of shock vector control using bypass flow passage," Journal of Heat and Fluid Flow, Vol. 62, pp. 474-481, (2016).
10. Kong, F., Jin, Y. and Kim, H.D. "Thrust vector control of supersonic nozzle flow using a moving plate," Journal of Mechanical Science and Technology, Vol. 30, No. 3, pp. 1209-1216, (2016).
11. Salemi, V.R., Sohrabi, S., Hojaji, M. and Soufivand, M.R., "Experimental study on the effects of secondary injection thrust vector in a Micro-Nozzles", First National Conference on Advances and Challenges in Engineering and Technology, Iran, (2016). (In Persian)
12. Salehifar, M., Tahani, M., Hojaji, M. and Dartoomian, A., "CFD modeling for flow field characterization and performance analysis of HGITVC", Applied Thermal Engineering, Vol. 103, pp. 291-304, (2016).
13. Mokhtari, D., Hojaji, M. and Mokhtari, M., "Experimental study of the effect of Protuberance on the thrust vector in convergent-divergent micro nozzle", 16th International Conference of Iranian Aerospace Society, Khaje Naseerdin Tousi University of Technology, Tehran, (2017). (In Persion)
14. Li, L., Hirota, M., Ouchi, K. and Saito, T., "Evaluation of fluidic thrust vectoring nozzle via thrust pitching angle and thrust pitching moment", Shock Waves, Vol. 27, No. 1, pp. 53-61, (2017).
15. Mokhtari, D., Hojaji, M. and Afrand, M., "Experimental investigation of the effect of cylindrical protuberance with different penetration the thrust vector a C-D nozzle in supersonic regime", Modares Mechanical Engineering, Vol. 19, No. 5, pp. 1145-1154, (2019).
16. Mokhtari, D., Hojaji, M. and Afrand, M., "Experimental investigation of the effect of location of cylindrical protuberance on the thrust vector of a supersonic C-D nozzle", Journal of Solid and Fluid Mechanics, Vol. 9, No. 1, pp. 237-249, (2019).
17. Babaeyan, M.R. and Hojaji, M., "Experimental investigation of the penetration effects of opposite dual protuberances on thrust vector of a supersonic C-D nozzle", Modares Mechanical Engineering, Vol. 19, No. 7, pp. 1741-1750, (2019).
18. Sharafi, A. and Mokhtari, D., "Experimental study of effect of obstacle presence and its geometry on thrust vector and outlet jet in a convergent-divergent micro nozzle", Modares Mechanical Engineering, Vol. 20, No. 5, pp. 1211-1221, (2020).
19. Tahani, M., Hojaji, M. and Mahmoodi, S.V., "Turbulent jet crossflow analysis with LES approach", Aircraft Engineering and Aerospace Technology, Vol. 88, No. 6, pp. 717-728, (2016).
ارسال نظر در مورد این مقاله