Zobrazeno 1 - 10
of 44
pro vyhledávání: '"R, Naren Shankar"'
Autor:
R., Naren Shankar, V.G., Ganesan
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2022, Vol. 94, Issue 10, pp. 1614-1627.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-02-2021-0050
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2021, Vol. 94, Issue 2, pp. 198-209.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-05-2021-0143
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2021, Vol. 93, Issue 7, pp. 1193-1203.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-10-2020-0225
Autor:
V., Kirubakaran, R., Naren Shankar
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2021, Vol. 93, Issue 5, pp. 915-924.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-02-2021-0042
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2020, Vol. 92, Issue 4, pp. 633-644.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-05-2019-0104
Autor:
R., Naren Shankar, S., Kevin Bennett
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2019, Vol. 91, Issue 9, pp. 1205-1213.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-01-2019-0007
Publikováno v:
International Journal of Vehicle Structures and Systems. 14
The study examines the quality of friction stir welded joints made with butt joints on a metal matrix composite. In the composite, AA6061 is the matrix and silicon carbide is the reinforcement. Joints were made with three different pin profiles: circ
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2398a6cdc11c9cb99a17cfcd17967439
https://doi.org/10.4273/ijvss.14.6.17
https://doi.org/10.4273/ijvss.14.6.17
Publikováno v:
Transdisciplinary Journal of Engineering & Science. 13
The current paper demonstrates the design parameters and tolerances for a horizontal axis wind turbine. Here we have adopted one of the DOE (design of experiment) method namely Taguchi method, a traditional approach for designing a robust wind turbin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7472196cd951f487c00287785c132bde
https://doi.org/10.22545/2022/00216
https://doi.org/10.22545/2022/00216
Publikováno v:
Aircraft Engineering and Aerospace Technology. 93:1193-1203
Purpose The effect of increasing lip thickness (LT) and Mach number on subsonic co-flowing Jet (CFJ) decay at subsonic and correctly expanded sonic Mach numbers has been analysed experimentally and numerically in this study. This study aims to a crit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::01232a9cbdd56744f4d3caf81fb1f292
https://doi.org/10.1108/aeat-10-2020-0225
https://doi.org/10.1108/aeat-10-2020-0225
Autor:
R. Naren Shankar, V Kirubakaran
Publikováno v:
Aircraft Engineering and Aerospace Technology. 93:915-924
Purpose This paper aims to predict the effect of combustor inlet area ratio (CIAR) on the lean blowout limit (LBO) of a swirl stabilized can-type micro gas turbine combustor having a thermal capacity of 3 kW. Design/methodology/approach The blowout l
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e7d520576dbfd3f232aac65d73d3b4b4
https://doi.org/10.1108/aeat-02-2021-0042
https://doi.org/10.1108/aeat-02-2021-0042