Zobrazeno 1 - 10
of 54
pro vyhledávání: '"Rajesh Sadanandan"'
Autor:
Rajesh Sadanandan
Publikováno v:
Flow, Turbulence and Combustion. 110:689-705
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fa2ee7f3e772ac137368f6de8c5cae77
https://doi.org/10.1007/s10494-022-00384-0
https://doi.org/10.1007/s10494-022-00384-0
Publikováno v:
25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ad604674ad3183b20c727d5d4892e606
https://doi.org/10.2514/6.2023-3044
https://doi.org/10.2514/6.2023-3044
Autor:
Aryadutt Oamjee, Rajesh Sadanandan
Publikováno v:
International Journal of Hydrogen Energy. 47:9408-9421
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f4569be75445a0702b25cbe88cb3344d
https://doi.org/10.1016/j.ijhydene.2022.01.022
https://doi.org/10.1016/j.ijhydene.2022.01.022
Publikováno v:
Proceedings of the Combustion Institute. 38:5209-5217
The effect of CO2 dilution on the flame characteristics and pollutant emission of a partially premixed CH4-air flame in a confined bluff body and swirl influenced flowfield is investigated using optical and laser diagnostic methods. The non-premixed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2aa0d03e1580b06bc36fc81f39223fde
https://doi.org/10.1016/j.proci.2020.06.153
https://doi.org/10.1016/j.proci.2020.06.153
Publikováno v:
Combustion Science and Technology. 194:1091-1107
Experimental investigation of a partially premixed flame stabilized in a combination of bluff body and swirling flowfields is reported. Simultaneous measurement of 2D fuel distribution (Acetone-PLI...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2e8fb7f923dc567f5c4553183c3f1157
https://doi.org/10.1080/00102202.2020.1802589
https://doi.org/10.1080/00102202.2020.1802589
Autor:
Rajesh Sadanandan, Aryadutt Oamjee
Publikováno v:
Combustion Science and Technology. 194:1044-1061
A comparative study is performed to investigate the effectiveness of non-reactive supersonic flow simulations in qualitatively predicting the mixing performance and flameholding capability of a pyl...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::148eef3a98ca0120d199abfbb0360e34
https://doi.org/10.1080/00102202.2020.1801657
https://doi.org/10.1080/00102202.2020.1801657
Publikováno v:
Journal of Applied Fluid Mechanics, Vol 13, Iss 3, Pp 839-847 (2020)
The objective was to study the effect of change in swirl intensities, S=0.4, 0.7 & 1 of the annular swirling flow on the exit flow field of an unconfined annular swirl burner operated at isothermal (only dry air) and reacting flow (premixed methane a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::39b6b620f025554104dbdc9ed71e7160
https://doi.org/10.29252/jafm.13.03.30646
https://doi.org/10.29252/jafm.13.03.30646
Autor:
Aryadutt Oamjee, Rajesh Sadanandan
Publikováno v:
The Aeronautical Journal. 124:1262-1280
Numerical investigation of the effect of pylon geometry within a pylon-cavity aided Supersonic Combustion Ramjet (SCRAMJET) combustor on mixing enhancement, flame-holding capability, fuel jet penetration and total pressure loss are conducted in the c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::78b24dcdd3d1cf7ea04d92764ccbcdd0
https://doi.org/10.1017/aer.2020.27
https://doi.org/10.1017/aer.2020.27
Publikováno v:
International Journal of Heat and Mass Transfer. 141:1140-1151
Experimental and numerical studies on the effect of heat transfer to an open cavity placed in supersonic crossflow are presented. Cavity floor is subjected to the desired amount of heat flux and the consequent effects in the flow dynamics inside the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::33fe36ff01851b333b7945a47377e8fb
https://doi.org/10.1016/j.ijheatmasstransfer.2019.07.058
https://doi.org/10.1016/j.ijheatmasstransfer.2019.07.058
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://explore.openaire.eu/search/publication?articleId=doi_dedup___::877d4f28e217f8d661f53693a9b603f9
https://doi.org/10.29252/jafm.12.05.29842
https://doi.org/10.29252/jafm.12.05.29842