Zobrazeno 1 - 6
of 6
pro vyhledávání: '"V S Saranyamol"'
Publikováno v:
Physics of Fluids. 35
A planar shock of initial strength MS = 3.0 was focused to a tiny region in space using a spherically converging test section. The shock accelerates inside the test section, collides with the focusing end wall, and gets reflected. Numerical studies s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::746f7a25bb233cf85674b9efe0cf25b8
https://doi.org/10.1063/5.0135618
https://doi.org/10.1063/5.0135618
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 235:1118-1126
Experimental studies on open cavity flows at supersonic speed of M = 2.0 were carried out. Oil flow visualization tests were made to understand the steady features of the surface flow field. Unsteady pressure measurements were done at five locations
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::51c104627471c9de4acf083f2f77068d
https://doi.org/10.1177/0954410020966493
https://doi.org/10.1177/0954410020966493
A detailed numerical study on the phenomenon of Shock Wave focusing in air is carried out. The focusing phenomenon is achieved with the help of a shock tube and a converging section attached to it. The planar shock generated inside the shock tube is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::82f576e5f24b1a595a9ebd0454cbecb3
Publikováno v:
Sustainable Development for Energy, Power, and Propulsion ISBN: 9789811556661
A large amount of energy is associated with shock waves. Current work studies the flow parameters upon exposure to cylindrical and spherical shock focusing. Shock wave is allowed to focus by traversing through a confined converging section attached t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81e92d59ded2a004e85d8487cf9734ed
https://doi.org/10.1007/978-981-15-5667-8_2
https://doi.org/10.1007/978-981-15-5667-8_2
Publikováno v:
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c44e5ef6160142b69ec7fae9b60f5293
https://doi.org/10.3850/978-981-11-2730-4_0144-cd
https://doi.org/10.3850/978-981-11-2730-4_0144-cd
Publikováno v:
Journal of Fluids Engineering. 140
Studies were made to understand the flow features around an open cavity at Mach 2.0 corresponding to Re = 0.55 × 106 based on the cavity depth. Experiments were carried out using a blowdown type supersonic wind tunnel having a test section size of 5
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d07e721eb74ca03b31a5a97b123fa9bf
https://doi.org/10.1115/1.4039247
https://doi.org/10.1115/1.4039247