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Naresh Relangi
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The Implication of Injection Locations in an Axisymmetric Cavity-Based Scramjet Combustor
N Relangi, A Ingenito, S Jeyakumar
Energies 14 (9), 2626, 2021
112021
Numerical simulations of axisymmetric aft wall angle cavity in supersonic combustion ramjets
N Relangi, D Garimella, K Jayaraman, J Venkatesan, S Jeyakumar, ...
Proceedings of the AIAA Propuls, Energy, 1-15, 2020
62020
The investigation of inclined aft wall cavities in a circular scramjet combustor
N Relangi, A Ingenito, S Jeyakumar
International Journal of Engine Research 24 (4), 1300-1311, 2023
52023
SHAR for a TSTO launcher
N Relangi, LNP Peri, A Ingenito
25th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2023
12023
Design of Supersonic and Hybrid engine based Advanced Rocket (SHAR)
N Relangi, LNP Peri, CHFL Domingos, A Fossella, JML Henriques, ...
IOP Conference Series: Materials Science and Engineering 1226 (1), 012031, 2022
12022
The implication of injection locations in an axisymmetric cavity-based scramjet combustor. Energies 2021; 14: 2626
N Relangi, A Ingenito, S Jeyakumar
s Note: MDPI stays neutral with regard to jurisdictional claims in published …, 2021
12021
Numerical investigations on the effect of injection locations in a cavity based axisymmetric scramjet combustor
N Relangi, A Ingenito, S Jeyakumar
AIP Conference Proceedings 2584 (1), 2023
2023
Computational Simulation of Axis Symmetric Aft Wall Angle Cavity in Supersonic Flow Field
N Relangi, D Garimella, K Jayaraman, J Venkatesan, S Jeyakumar, ...
AIAA Propulsion and Energy 2020 Forum, 3712, 2020
2020
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