Optimization of Thrust Coefficient in Baseline and Ribbed Convergent–Divergent  Nozzles

Kunal Pansari  , Ajay Kumar Verma , Vikas Kumar Sukhdeve  , D. N. Dewangan

Optimization of Thrust Coefficient in Baseline and Ribbed Convergent–Divergent Nozzles

Authors

Kunal Pansari , Ajay Kumar Verma , Vikas Kumar Sukhdeve , D. N. Dewangan

Keywords:

C-D Nozzle; Thrust Coefficient; CFD; Ribbed Nozzles; Taguchi; Optimization

Abstract

This study investigates the aerodynamic performance and optimization of four convergent–divergent (C–D)rocket nozzles RN–1 (baseline), RN–2 (circular rib), RN–3 (isosceles rib), and RN–4 (scalene rib) usingComputational Fluid Dynamics (CFD) and Taguchi-based design of experiments (DOE). The thrust coefficient (CF) is adopted

References

Shaji S, Radhakrishnan V. Analysis of process parameters in surface grinding with graphite as lubricant based on the Taguchi method. J Mater Process Technol 2003;141(1):51–9

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Published

2024-06-20

How to Cite

Kunal Pansari , Ajay Kumar Verma , Vikas Kumar Sukhdeve , D. N. Dewangan. (2024). Optimization of Thrust Coefficient in Baseline and Ribbed Convergent–Divergent Nozzles. Journal of Computational Analysis and Applications (JoCAAA), 33(06), 3496–3509. Retrieved from https://www.eudoxuspress.com/index.php/pub/article/view/3998