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Naren Shankar
Naren Shankar
Associate Professor (Research), Aeronautical Engineering, Vel Tech Rangarajan Dr. Sagunthala R&D
Verified email at veltech.edu.in
Title
Cited by
Cited by
Year
Ultimate strength prediction of carbon/epoxy tensile specimens from acoustic emission data
V Arumugam, R Naren Shankar, BTN Sridhar, AJ Stanley
Journal of Materials Science & Technology 26 (8), 725-729, 2010
462010
Numerical characterization of lip thickness on subsonic and correctly expanded sonic co-flowing jets
R Naren Shankar, S Thanigaiarasu, E Rathakrishnan
Transactions of the japan society for aeronautical and space sciences 59 (3 …, 2016
242016
Influence of bypass ratio on subsonic and correctly expanded sonic co-flowing jets with finite lip thickness
S Thanigaiarasu, R Naren Shankar, E Rathakrishnan
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2019
192019
Co-Flowing Jet Control Using Lip Thickness Variation
R Naren Shankar, S Thanigaiarasu, S Elangovan, E Rathakrishnan
International Journal of Turbo and Jet Engines 38 (3), 289 - 302, 2021
182021
Characteristics of a co-flowing jet with varying lip thickness and constant bypass ratio
R Naren Shankar, S Kevin Bennett
Aircraft Engineering and Aerospace Technology 91 (9), 1205-1213, 2019
17*2019
Characteristics of a co-flowing jet with varying lip thickness and constant velocity ratio
R Naren Shankar, SK Bennett, ND Raja, KS Kumar
Aircraft Engineering and Aerospace Technology 92 (4), 633-644, 2020
132020
Novel Characteristics of Subsonic Coflowing Jets With Varying Lip Thickness
R Naren Shankar, N Dilip Raja
Journal of Aerospace Technology and Management 12 (e2520), 1-13, 2020
9*2020
Semi-circular corrugated tabs to control subsonic and correctly expanded sonic jets
K Sathish Kumar, C Senthilkumar, R Naren Shankar
Aircraft Engineering and Aerospace Technology 93 (6), 1076-1084, 2021
8*2021
Design and fabrication of horizontal axis wind turbine
RN Shankar, LR Kumar, MV Ramana
2016 IEEE students’ conference on electrical, electronics and computer …, 2016
72016
Statistical Analysis using Taguchi Method for Designing a Robust Wind Turbine
V Kaushik, N Shankar
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences 100 (3 …, 2022
52022
Effect of lip thickness and bypass co-flowing jets
R Naren Shankar
Ph. D. thesis, Anna University, 2017
52017
Optimization of friction STIR welded AA6061+ SiCp metal matrix composite to increase joint tensile strength and reduce defects
ND Raja, RN Shankar
International Journal for Simulation and Multidisciplinary Design …, 2021
42021
Numerical Study on Supersonic Co-flowing Jet with Varying Lip Thickness
S R. Naren, K K. Sathish, R N. Dilip, CS Kamal Raj, NK Raj, D Gupta
Innovative Design, Analysis and Development Practices in Aerospace and …, 2021
42021
Evaluation of efficiency of double slope solar still and drinking water yield using silver nanoparticle mixed with phase change material
MI Shajahan, DR Narayana, NS Radha Krishnan, JJ Michael
Energy Sources, Part A: Recovery, Utilization, and Environmental Effects 44 …, 2022
32022
Numerical analysis of supersonic co-flow jet with varying lip thickness
K Sathish Kumar, R Naren Shankar, K Anusindhiya, BR Senthil Kumar
Aircraft Engineering and Aerospace Technology, ahead-of-print, 2021
3*2021
Review of Experimental Approaches for the Analysis of Aerodynamic Performance of Vertical Axis Wind Turbines
V Kaushik, RN Shankar
Innovative Design, Analysis and Development Practices in Aerospace and …, 2021
32021
Numerical Study on Sonic Underexpanded Co-flowing Jet with Varying Separation Distance
RN Shankar, KS Kumar, ND Raja, J Sumendran, NK Raj, PK Yadav, ...
Innovative Design, Analysis and Development Practices in Aerospace and …, 2021
3*2021
Jet noise reduction in co-flowing jets with finite lip thickness
SK Bennett, RN Shankar
International Journal of Vehicle Structures & Systems 12 (4), 476-480, 2020
32020
Numerical investigation of critical lip thickness of subsonic co-flowing jet
R Naren Shankar, VG Ganesan, N Dilip Raja, K Sathish Kumar, ...
Aircraft Engineering and Aerospace Technology 93 (7), 1193 - 1203, 2021
22021
Effect of lip thickness and bypass ratio on characteristics of co-flowing jets
R Naren Shankar
PhD Thesis, Anna University, India, 2017
22017
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