Open Access
| Issue |
E3S Web Conf.
Volume 477, 2024
International Conference on Smart Technologies and Applied Research (STAR'2023)
|
|
|---|---|---|
| Article Number | 00027 | |
| Number of page(s) | 11 | |
| DOI | https://doi.org/10.1051/e3sconf/202447700027 | |
| Published online | 16 January 2024 | |
- Krishna Murari Pandey, Surendra Yadav, CFD Analysis of a Rocket Nozzle with FourInlets at Mach 2.1 International Journal of Chemical Engineering and Applications 2020 vol. 1(no. 4):pp. 319-325. [Google Scholar]
- K. Sankari Ashok Alshiya, M. Santhosh, V.K. Santhosh, S. Sai Gopal, Experimental analysis of jet flow in an aerospike nozzle, Materials Today proceedings Volume 46, Part 9, 2021, Pages 3444-3450 [CrossRef] [Google Scholar]
- K.M. Pandey and S.K. Yadav, ,CFD Analysis of a Rocket Nozzle with Two Inlets at Mach. 1,vJournal of Environmental Research and Development, Vol 5, No 2,2010, (pp 308-321. [Google Scholar]
- P. Padmanathan, Dr. S. Vaidyanathan, Computational Analysis of Shockwave in Convergent Divergent Nozzle, International Journal of Engineering Research and Applications (IJERA), Vol. 2, Issue 2, Mar-Apr 2012, pp.1597-1605. [Google Scholar]
- Natta, Pardhasaradhi.; Kumar, V. Ranjith.; Rao, Dr. Y.V. Hanumantha; Flow Analysis of Rocket Nozzle Using Computational Fluid Dynamics (Cfd), International Journal of Engineering Research and Applications (IJERA), Vol. 2, Issue 5, September- October 2012, pp.1226-1235. [Google Scholar]
- Pandey,K.M.; Singh, A.P.; CFD Analysis of Conical Nozzle for Mach 3 at V arious Angles of Divergence with Fluent Software, International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010, 179-185. [CrossRef] [Google Scholar]
- Madhu B P, Syed Sameer, Kalyana Kumar M, Mahendra Mani G; “CFD Analysis Of Convergent divergent And Contour Nozzle” International Journal of Mechanical Engineering and Technology (IJMET) Volume 8, Issue 8, August 2017, pp. 670–677, [Google Scholar]
- S. Srikrishnan and Dr. P. K. Dash. 2D CFD Analysis of Deflagration to Detonation Transition in Closed Pip e Using Different Blockage. International Journal of Mechanical Engineering and Technology, 8(6), 2017, pp. 447–454. [Google Scholar]
- K. Manikandan, Jishu Chandran, A. Devaraj and R. Ganesh. A CFD Analysis for Optimization of Total Disolved Solids in Impeller Mixing Solid Waste Anaerobic Digester. International Journal of Mechanical Engineering and Technology, 8(7), 2017, pp. 283–289. [Google Scholar]
- Muhammad Waqas Khalid, Muhammad Ahsan omputational 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, 2020, 5180-5185 [CrossRef] [Google Scholar]
- Shaik Khaja Hussain, V Amarnath Reddy, V Hari Babu, Modelling and Computational Fluid Dynamic Analysis on Jet Nozzle. IJSDR(2016) | Volume 1, Issue 9,416-425. [Google Scholar]
- Prosun Roy, Abhijit Mondal, Biswanath Barai, Design and Analysis Of Rocket Engine Nozzle by using CFD and Optimization of Nozzle parameters, International Journal of Advanced Engineering Research and Science (IJAERS), Vol-3, Issue-1, Jan- 2016] 39-46. [Google Scholar]
- Jatuporn Thongsri, Kamonwan Srathonghuam & Adulyasak Boonpan Gas Flow and Ablation of 122 mm Supersonic Rocket Nozzle Investigated by Conjugate Heat Transfer Analysis, Processes 2022, 10(9), 18-23 [Google Scholar]
- Gutti Rajeswara Rao,U.S. Ramakanth, A. Lakshman, Flow Analysis in a Convergent-Divergent Nozzle Using CFD, International Journal of Research in Mechanical Engineering Volume 1, Issue 2, October- December, 2013, pp.136-144,. [Google Scholar]
- Shaik Khaja Hussain, 2B V Amarnath Reddy, 3A V Hari Babu. Modelling and Computational Fluid Dynamic Analysis on Jet Nozzle. International Journal of Scientific Development and Research September 2016 Volume 1, Issue 9.416-425 [Google Scholar]
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