Zobrazeno 1 - 10
of 36
pro vyhledávání: '"Ashok K. Barik"'
Publikováno v:
JP Journal of Heat and Mass Transfer. 30:75-88
Autor:
Prafulla Kumar Swain, Siva Prasad Dora, Suryanarayana Murthy Batulla, Shoba Chintada, Ashok K. Barik
Publikováno v:
Archive of Applied Mechanics. 92:1149-1156
Autor:
Rama Chandra Panda, Sudhansu S. Sahoo, Ashok K. Barik, Debjyoti Sahu, Taraprasad Mohapatra, Auroshis Rout
Publikováno v:
Recent Advances in Thermofluids and Manufacturing Engineering ISBN: 9789811943874
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::852a8daf198fa938d31414313f001a31
https://doi.org/10.1007/978-981-19-4388-1_30
https://doi.org/10.1007/978-981-19-4388-1_30
Autor:
Sachin K. Mishra, Ashok K. Barik
Publikováno v:
Journal of Heat Transfer. 144
Infrared suppression devices (IRS) are frequently used in naval/cargo ships to passively entrain an additional amount of cold air from the atmosphere, and mix it with the hot plume so as to suppress its temperature, and the IR signature. In this work
Autor:
Prafulla Kumar Swain, Challa Balaji Naga Sai Abhishikt, Ganti Naga Alekhya, Siva Prasad Dora, Ashok K. Barik
Publikováno v:
Journal of Offshore Mechanics and Arctic Engineering. 145
In the present research, a 2D simulation of tandem flapping foil following an elliptical trajectory, i.e., altered from a simple flapping trajectory is performed. The purpose of the research is to evaluate the influence of the trajectory motion of th
Publikováno v:
Journal of Thermal Science and Engineering Applications. 14
A passive infrared suppression (IRS) device is an important and integral part of the modern naval/cargo ships, fighter jets, and helicopters to cool down the hot exhaust gas to suppress the infrared (IR) signatures. A modified IRS device has been pro
Publikováno v:
International Communications in Heat and Mass Transfer. 145:106817
Autor:
Ashok K. Barik, Manoj Kumar Dash
Publikováno v:
International Journal of Thermal Sciences. 187:108196
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 235:1648-1663
The present research focuses on the timing of wing–wing interaction that benefits the aerodynamic force of a dragonfly in hovering flight at Reynolds number 1350. A 3-D numerical simulation method, called the system coupling, was utilised by implem
Publikováno v:
Ocean Engineering. 268:113390