[1] G. Cican, V. Stanciu and D. Crunteanu,” Analytical and Numerical Study of the Nozzle Jet”, UPB Scientific Bulletin, Series D: Mechanical Engineering, Vol. 76, No. 1, pp: 37-44, 2014.
[2] V. Tapasvi, M.S. Gupta and T. Kumaraswamy, “Designing and Simulating Compressible Flow in a Nozzle”, International Journal of Engineering and Advanced Technology, Vol. 4, No. 6, pp: 46-54, 2015.
[3] O.J. Shariatzadeh, A. Abrishamkar and A.J. Jafari, “Computational Modeling of a Typical Supersonic Converging-Diverging Nozzle and Validation By Real Measured Data”, Journal of Clean Energy Technologies, Vol. 3, No. 3, pp: 220-225, 2015.
[4] V. Ramji, R. Mukesh, and H. Inamul, “Design and Numerical Simulation of Convergent Divergent Nozzle”, Applied Mechanics and Materials, Vol. 852, pp: 617-624, 2016.
[5] A. Balabel, A.M. Hegab, M. Nasr, and S.M. El-Behery, ”Assessment of Turbulence Modeling for Gas Flow in Two-Dimensional Convergent–Divergent Rocket Nozzle”, Applied Mathematical Modelling, Vol. 35, pp: 3408–3422, 2011.
[6] M. Susila, N. Akhil, J.A. Tennyson and Gh. Somnath, ”Large-Eddy Simulation of Compressible Turbulent Flow in Convergent-Divergent Nozzles with Isothermal Wall”, International Journal of Heat and Fluid Flow, Vol. 78, 2019.
[7] M.W. Khalid, and M. Ahsan, “Computational Fluid Dynamics Analysis of Compressible Flow Through a Converging Diverging Nozzle Using the K-ε Turbulence Model”, Engineering, Technology & Applied Science Research, Vol, 10, No. 1, pp: 5180-5185, 2020.
[8] B.P. Madhu, S. Syed, K.M. Kalyana, and G. Mahendra Mani, “CFD Analysis of Convergent-Divergent and Contour Nozzle”, International Journal of Mechanical Engineering and Technology, Vol. 8, No. 8, pp: 670-677, 2017.
[9] A. Khan, A. Aabid, and S.A. Khan, “CFD Analysis of Convergent-Divergent Nozzle Flow and Base Pressure Control Using Micro-JETS”, International Journal of Engineering & Technology, Vol. 7, No. 3.29, pp: 232-235, 2018.
[10] K.A. Pathan, S.A. Khan, and P.S. Dabeer, “CFD Analysis of Effect of Mach Number, Area Ratio and Nozzle Pressure Ratio on Velocity for Suddenly Expanded Flows”, Proceedings of the IEEE , pp:1104-1110, 2017.
[11] M.H. Hamedi-Estakhrsar, H. Mahdavy-Moghaddam, and M. Jahromi, “Investigation of Effects of Convergence and Divergence Half-Angles on the Performance of a Nozzle for Different Operating Conditions”, Journal of the Brazilian Society of Mechanical Sciences and Engineering, Vol. 40, No. 353, 2018.
[12] A.S. Swaroopini, M.G. Kumar and T.N. Kumar, “Numerical Simulation and Optimization of High Performance Supersonic Nozzle at Different Conical Angles”, International Journal of Research in Engineering and Technology, Vol. 4, No, 9, pp: 268-273, 2015.
[13] K. Bhide, K. Siddappaji, and Sh. Abdallah, “Aspect ratio Driven Relationship between Nozzle Internal Flow and Supersonic Jet Mixing”, Aerospace, Vol. 8, No. 78, 2021.
[14] I. Olaru, “A Study of Fluid Flow Simulation in Convergent-Divergent Nozzles”, Materials Science and Engineering, Vol. 95, No. 012048, 2015.
[16] N. Akbar Najjar, D. Dandotiya, and A. Najar,
Farooq ., “Comparative Analysis of K-ε and Spalart-Allmaras Turbulence Models for
Compressible Flow through a Convergent-Divergent Nozzle”,
The International Journal Of Engineering And Science, Vol. 2, No. 8, pp: 08-17, 2013.
[17] P. R. Spalart and S. R. Allmaras, “A One Equation Turbulence Model for Aerodynamic Flows”, Recherche Aerospatiale, Vol. 1, pp: 5-21, 1994.
[18] R. Ranjan, S. K. chou, F. Riaz and K. Kartikeian, “Cold gas micro propulsion development for satellite application”, Energy Procedia, Vol. 143, pp. 754-761, 2017.