Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Abu Taher Ali"'
Autor:
Shams Sourav, Md. Abu Taher Ali
Publikováno v:
European Journal of Engineering and Technology Research. 7:18-24
Flow field characteristics of a free circular swirling jet are investigated in the present study considering three different swirl numbers 0.38, 0.56 and 0.80. The experiment is carried out in an air jet facility for Reynolds numbers 16300, 34400 and
Publikováno v:
Journal of Mechanical Engineering, Automation and Control Systems. 2:36-43
The phenomena of mean pressure distribution around two square cylinders in tandem has been carried out. Also the mean velocity distribution in the wake of the two cylinder are studies. The Navier-Stokes equation for conservation of momentum and the c
Publikováno v:
European Journal of Engineering and Technology Research. 5:140-144
Two parallel pipe jets of 20 mm diameter were placed 1.2 mm diameter apart and were connected by a 4 mm wide channel all along the central plane of the jets. The mean velocity flow field of the jets was investigated for three Reynolds number 16300, 3
Publikováno v:
European Journal of Engineering Research and Science. 5:1199-1203
In this investigation experiment was carried out in 80 mm diameter swirling pipe jet, where swirl was generated by attaching wedge-shaped helixes in the pipe. All measurements were taken at Re 5.3e4. In the plain pipe jet the potential core was found
Publikováno v:
Proceedings of the 13th International Conference on Mechanical Engineering (ICME2019).
In this investigation experiment was carried out on a 50mm diameter pipe jet fitted at the jet flow setup. Measurements were taken at Re 1.125e5 and 0.75e5 based on the diameter of the pipe jet. Measurements were taken with three-hole wedge type yawm
Publikováno v:
AIP Conference Proceedings.
In the present investigation mean flow parameters of 50mm diameter circular swirling jet are measured with 3-hole wedge shaped yaw meter. In this experiment three nozzles are used and these are for free jet, for 30 degree swirl jet and for 45 degree
Autor:
Md. Arif Hassan Mamun, A.K.M. Sadrul Islam, Md. Abu. Taher Ali, G.M. Jahangir Alam, Md. Quamrul Islam
Publikováno v:
Procedia Engineering. :225-231
This paper explains the fabrication of an UAV having aerofoil shaped fuselage using NACA 4416 profile and compare the result between the aerodynamic characteristics with that of the same model obtained from CFD investigation. Open circuit subsonic wi