Zobrazeno 1 - 10
of 205
pro vyhledávání: '"Ethirajan Rathakrishnan"'
Autor:
Scwartz, Irish Angelin, Rathakrishnan, Naren Shankar, Kumar, Sathish Kumar, Kengaiah, Vijayaraja, Ethirajan, Rathakrishnan
Publikováno v:
International Journal of Turbo & Jet-Engines; Aug2024, Vol. 41 Issue 3, p645-657, 13p
Akademický článek
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Autor:
Ethirajan Rathakrishnan
Publikováno v:
The Aeronautical Journal. :1-13
This paper presents the results of the experimental study carried out to address the issues of base heating and smooth separation of the stage of launch vehicles. The pressure at the base of a convergent-divergent circular nozzle, from which Mach 1.8
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0456bca2e957efbafe59b4da0842ab9f
https://doi.org/10.1017/aer.2023.13
https://doi.org/10.1017/aer.2023.13
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 237:1571-1581
The jet mixing caused by two rectangular and triangular tabs of geometric blockage 2.5% each, separated by 90⁰ at the nozzle exit plane of a Mach 2 circular jet, in the presence of varying levels of expansion, corresponding to nozzle pressure ratio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::985be7c6302e83d8de000661a4a3cafd
https://doi.org/10.1177/09544100221132653
https://doi.org/10.1177/09544100221132653
Publikováno v:
AIAA Journal. 60:6054-6061
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0ee4c1798a47b38910ab72d05f5b5fe8
https://doi.org/10.2514/1.j061786
https://doi.org/10.2514/1.j061786
Publikováno v:
AIAA Journal. 60:4639-4648
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d8f11612e45a8bcff23a9b5714bb630e
https://doi.org/10.2514/1.j061257
https://doi.org/10.2514/1.j061257
Akademický článek
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Autor:
Naren Shankar Radha Krishnan, Sathish Kumar Kumar, Vijayaraja Kengaiah, Senthilkumar Chidambaram, Ethirajan Rathakrishnan
Publikováno v:
International Journal of Turbo & Jet-Engines.
The characteristics of a sonic under-expanded coaxial jet with lip thickness 1.5D p (where D p is the exit diameter of primary jet equals 10 mm) with the primary jet operating at nozzle pressure ratio (NPR) of 3, 4 and 5. For NPR 3 operating primary
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ac4f820089029d493153f1c6297cfd34
https://doi.org/10.1515/tjj-2022-0068
https://doi.org/10.1515/tjj-2022-0068
Publikováno v:
Iranian Journal of Science and Technology, Transactions of Mechanical Engineering. 46:407-420
Effect of eccentricity on jets delivered from a primary nozzle surrounded by secondary flow is studied experimentally. The eccentricity is achieved by offsetting the annular spacing of the co-flow passage, surrounding the center nozzle generating the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::250951509f1001c97cba6f1733fb4e63
https://doi.org/10.1007/s40997-021-00444-2
https://doi.org/10.1007/s40997-021-00444-2