Zobrazeno 1 - 10
of 108
pro vyhledávání: '"M, Deepu"'
Autor:
S. Jayakrishnan, M. Deepu
Publikováno v:
Journal of Applied Fluid Mechanics, Vol 14, Iss 1, Pp 49-59 (2021)
Numerical simulation of the supersonic turbulent reacting flow field in a dual throat- dual fuel rocket thrust chamber is presented. Future single stage to orbit and high lift space transportation missions aspire a reliable, efficient, and cost-effec
Externí odkaz:
https://doaj.org/article/7d87c04270da4e8185e1a8db32c1de24
Publikováno v:
Journal of Applied Fluid Mechanics, Vol 12, Iss 5, Pp 1719-1728 (2019)
Thrust augmentation in rocket engines using secondary injection in the diverging part of a nozzle is an innovative extension of after burners. This technique finds application in single stage to orbit propulsion devices, where the nozzle has to work
Externí odkaz:
https://doaj.org/article/86e2c2c46c3e4e6e86e0aac2cbde6ce4
Autor:
P, Shivakumar, M, Deepu, M N, Monika, K S, Manjunatha Kumara, Budagumpi, Srinivasa, Nagaraju, D H
Publikováno v:
Energy & Fuels; 4/4/2024, Vol. 38 Issue 7, p6281-6289, 9p
Autor:
Sathiyanarayanan, T., Vijay M., Deepu
Publikováno v:
In Power Systems Operation with 100% Renewable Energy Sources 2024:55-64
Publikováno v:
Journal of Applied Fluid Mechanics, Vol 10, Iss 6, Pp 1605-1614 (2017)
Single stage to orbit propulsion devices are being developed as part of low cost access to space endeavors. Sea level operation of high area ratio rocket nozzle used in rocket engines leads to an overexpanded flow condition resulting in high side loa
Externí odkaz:
https://doaj.org/article/ff6356d48b32474a974bc4b630d5695d
Publikováno v:
Journal of Enhanced Heat Transfer. 29:49-67
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::487c5d2d658e36b52796e335d14097db
https://doi.org/10.1615/jenhheattransf.2022040635
https://doi.org/10.1615/jenhheattransf.2022040635
Autor:
M. Deepu, S. Jayakrishnan
Publikováno v:
Shock Waves. 31:929-943
Numerical simulation of the shock transitions during off-design operation of a dual throat nozzle (DTN) is presented. The DTN is a typical passive-altitude-compensation nozzle that exhibits a unique shock transition process during its thrust chambers
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2dc30a89d949faef5af05d13272e2517
https://doi.org/10.1007/s00193-021-01037-3
https://doi.org/10.1007/s00193-021-01037-3
Publikováno v:
Thermal Science and Engineering Progress. 42:101886
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7fd77432119b51a0bef1ea4a6027eb12
https://doi.org/10.1016/j.tsep.2023.101886
https://doi.org/10.1016/j.tsep.2023.101886
Publikováno v:
Journal of Thermal Science and Engineering Applications. 14
Numerical studies on the flow and heat transfer characteristics of rectangular regenerative cooling passages with lateral curvature for a high-area-ratio nozzle are presented. Unlike regular geometries of coolant paths used in various engineering app
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c163e290760b19061db678a25345628c
https://doi.org/10.1115/1.4054211
https://doi.org/10.1115/1.4054211
Publikováno v:
Journal of The Institution of Engineers (India): Series C. 101:661-670
A 3-D, steady, conjugate numerical model is used to study the effect of waviness on laminar fluid flow and heat transfer characteristics associated with microsized wavy channels. The numerical model has been validated against available experimental d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9c5f078ac3ec990e6688f97922409d80
https://doi.org/10.1007/s40032-020-00575-6
https://doi.org/10.1007/s40032-020-00575-6