Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Vignesh Ram Petha Sethuraman"'
Publikováno v:
Case Studies in Thermal Engineering, Vol 45, Iss , Pp 102947- (2023)
An equilibrium constant is an important parameter in regard to determining the backward reaction rate constant in chemical kinetics modeling for a hypersonic flow. Three common approaches for the equilibrium constant determination are based on the pa
Externí odkaz:
https://doaj.org/article/02e39ddbc5024a76ae610761ea301cbb
Autor:
S. Suganthi, Khuloud A. Alibrahim, S. Senthil Kumar, P. Saminathan, Abdullah Alodhayb, B. Aneeba, Vignesh Ram Petha Sethuraman, M.R. Muthumareeswaran
Publikováno v:
Journal of King Saud University: Science, Vol 35, Iss 3, Pp 102497- (2023)
Background: The micro-sieves filter out the suspended solid particles and microorganisms from the sample fluids such as water, blood samples, etc. Water is the most essential element among all the natural resources. It gets polluted as it flows and c
Externí odkaz:
https://doaj.org/article/5519c90691814ff9be1b3e8667bed17b
Publikováno v:
Acta Astronautica. 193:75-89
Autor:
Mannat Sharma, Aishwarya M. Upadhye, Piyush Munishwar, Satvi Sanghani, Vignesh Ram Petha Sethuraman, Devabrata Sahoo
Publikováno v:
AIAA SCITECH 2023 Forum.
The interaction between the self-excited shock train flow and the cavity shear layer in a scramjet isolator is investigated numerically using detached-eddy simulations (DES). The effect of changing the position of the shock train by controlling the b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f97f8f92e1bccb2d205623c2b4222820
http://arxiv.org/abs/2212.01718
http://arxiv.org/abs/2212.01718
Autor:
James, Jintu K.1 (AUTHOR), Vignesh Ram, Petha Sethuraman2 (AUTHOR), Kim, Heuy Dong1 (AUTHOR) kimhd@anu.ac.kr
Publikováno v:
Acta Astronautica. Feb2023, Vol. 203, p1-15. 15p.
Publikováno v:
Physics of Fluids. 34:016105
Publikováno v:
Aerospace Science and Technology. 118:107012
The isolator plays a major role in the scramjet engine by providing suitable pressure for the combustion process. It is situated between the inlet and the combustion chamber. The deceleration of supersonic flow into subsonic flow is achieved by a ser