Design and performance investigations on UAV’s convergent-divergent nozzle through validated computational aerodynamic simulation-Reference-Cited by-同舟云学术

Design and performance investigations on UAV’s convergent-divergent nozzle through validated computational aerodynamic simulation

Published:2022 Issue: Volume: Page:
ISSN:0094-243X
Container-title:THE 8TH ANNUAL INTERNATIONAL SEMINAR ON TRENDS IN SCIENCE AND SCIENCE EDUCATION (AISTSSE) 2021
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Author:

Prakash R. Arul,Kumar M. Senthil,Vijayanandh R.,Kumar K. Naveen,Prathap M.,Aswanth S.,Ajithkumar A.,Jagadeeshwaran P.

Publisher

AIP Publishing

Link

http://aip.scitation.org/doi/pdf/10.1063/5.0108306

Reference28 articles.

1. Arul Prakash. R et al., Design Optimization Of Convergent - Divergent Nozzle Using Computational Fluid Dynamics Approach, International Journal of Mechanical and Production Engineering Research and Development, ISSN(E): 2249-8001 Vol. 9, Special Issue 1, 220-232, 2019.

2. REMOVED

3. R Manivel, R Vijayanandh, T Babin and G Sriram, 2nd International Conference on Condensed Matter and Applied Physics (ICC 2017), AIP Conf. Proc. 1953, 140063-1–140063-5; https://doi.org/10.1063/1.5033238.

4. Senthil Kumar M et al., Conceptual Design and Comparative Computational Analysis of Secondary inlet of Rotary-wing Aircraft Engine, Journal of Advanced Research in Dynamical and Control Systems, Vol. 9. Sp– 14, pp 1189 – 1209, 2017.

5. E. Indhumathi, S. Pradesh, Vijayanandh. R, Senthil Kumar. M, Naveen Kumar. R & Raj Kumar. G, Comparative Computational Thermal Analysis Of Gas Turbine Engine Turbine-Blade Coated With And Without Lanthanum Zirconate, International Journal of Mechanical and Production Engineering Research and Development, ISSN(E): 2249-8001, Vol. 8, Special Issue 7, 1079–1088, 2018.