Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Aryadutt Oamjee"'
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
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
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
Autor:
Rajesh Sadanandan, Aryadutt Oamjee
Publikováno v:
Aerospace Science and Technology. 92:869-880
The current study numerically investigates the effect of fuel injection locations within a pylon-cavity aided Supersonic Combustion Ramjet (SCRAMJET) combustor on mixing enhancement, flame holding, fuel jet penetration and total pressure loss. RANS e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::72553aa218ef662f0db420dd85727226
https://doi.org/10.1016/j.ast.2019.07.021
https://doi.org/10.1016/j.ast.2019.07.021
Autor:
Rajesh Sadanandan, Aryadutt Oamjee
Publikováno v:
Physics of Fluids. 32:116108
A numerical investigation on the effects of fuel injection angle on various mixing parameters within a pylon-cavity aided supersonic combustor flameholder under non-reactive flow conditions is performed. The computational model based on Reynolds-aver
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5955489ab65c851c82cb21267117ccd8
https://doi.org/10.1063/5.0026125
https://doi.org/10.1063/5.0026125