Zobrazeno 1 - 10
of 46
pro vyhledávání: '"B. T. Kannan"'
Autor:
Mohan Vijaya Anoop, B. T. Kannan
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 236:1532-1545
A strategy for calibration of X-wire probes and data inversion is described in this article. The approach used has elements of full velocity vs yaw-angle calibration with robust curve fitting. The responses of an X-wire probe placed in a calibration
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2238fa35df032a39c438f0ccede1119f
https://doi.org/10.1177/09544100211040305
https://doi.org/10.1177/09544100211040305
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811913877
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f916a0ac688c5dce78dc0d3cb64ed8f2
https://doi.org/10.1007/978-981-19-1388-4_3
https://doi.org/10.1007/978-981-19-1388-4_3
Publikováno v:
Aircraft Engineering and Aerospace Technology. 93:42-50
Purpose The purpose of this study is to experimentally investigate the trends in shock wave Mach number that were observed when different diaphragm material combinations were used in the small-scale shock tube. Design/methodology/approach A small-sca
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79c7ecde5fbc040ba9639f3081eb440b
https://doi.org/10.1108/aeat-07-2019-0148
https://doi.org/10.1108/aeat-07-2019-0148
Publikováno v:
THE 8TH ANNUAL INTERNATIONAL SEMINAR ON TRENDS IN SCIENCE AND SCIENCE EDUCATION (AISTSSE) 2021.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::70400879cd7cc49742c6305acbe269b3
https://doi.org/10.1063/5.0118753
https://doi.org/10.1063/5.0118753
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811628993
2D flow analysis of a race car wing operating in the wake of varying diffuser angles is carried out in ANSYS Fluent CFD software. The combined effect of the high lift wing and the diffuser was studied in the wake region as it directly affects any veh
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b68981069496613b95cc1c1b5ce5565a
https://doi.org/10.1007/978-981-16-2900-6_8
https://doi.org/10.1007/978-981-16-2900-6_8
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811544873
Shock waves are a phenomenon that can be produced under constrained conditions inside a shock tube. These waves have a wide scope of studies due to their multi-disciplinary applications. Therefore, in the present work, the main focus is to conduct tr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::60650931afbc915381f36341113fcfed
https://doi.org/10.1007/978-981-15-4488-0_27
https://doi.org/10.1007/978-981-15-4488-0_27
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811547447
Smoldering is flameless combustion that occurs on the surface of the condensed phase that is very difficult to detect and which causes serious fire risks in residential and industrial areas by the presence of turbulent winds. Statistics show that maj
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bf3067841bd42410e73ff1bd8db1fe48
https://doi.org/10.1007/978-981-15-4745-4_90
https://doi.org/10.1007/978-981-15-4745-4_90
Publikováno v:
AIAA Propulsion and Energy 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b8c47c29dd30cc753ab5e53d769e0d23
https://doi.org/10.2514/6.2020-3648
https://doi.org/10.2514/6.2020-3648
Publikováno v:
Arabian Journal for Science and Engineering. 44:1475-1488
Two-dimensional numerical investigations on the flow characteristics past a circular cylinder with a jet injection at the rear stagnation point are performed. Transient, incompressible, laminar, and isothermal flow governing equations are solved with
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::21c8df2dc75726adef0bec2cdd39eae8
https://doi.org/10.1007/s13369-018-3588-1
https://doi.org/10.1007/s13369-018-3588-1
Autor:
B. T. Kannan, N R Panchapakesan
Publikováno v:
Aircraft Engineering and Aerospace Technology. 90:452-460
Purpose This study aims to investigate the effects of nozzle momentum flux distribution on the flow field characteristics. Design/methodology/approach The nozzle configuration consists of a central nozzle surrounded by four nozzles. All nozzles have
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b7f1d61509d9c1bf85e1d26dcc3033d
https://doi.org/10.1108/aeat-11-2016-0233
https://doi.org/10.1108/aeat-11-2016-0233