Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Md Saddam Hossain Joy"'
Autor:
Umnia Doha, Onur Aydin, Md Saddam Hossain Joy, Bashar Emon, William Drennan, M. Taher A. Saif
Publikováno v:
Acta biomaterialia. 154
Cells in functional tissues execute various collective activities to achieve diverse ordered processes including wound healing, organogenesis, and tumor formation. How a group of individually operating cells initiate such complex collective processes
Publikováno v:
SSRN Electronic Journal.
Autor:
Zhengwei Li, William C Balance, Md Saddam Hossain Joy, Shrey Patel, Joanne Hwang, Hyunjoon Kong, M Taher A Saif
Publikováno v:
Biofabrication. 14:025009
Tissue-engineered living machines is an emerging discipline that employs complex interactions between living cells and engineered scaffolds to self-assemble biohybrid systems for diverse scientific research and technological applications. Here, we re
Publikováno v:
AIP Conference Proceedings.
In the present study, a numerical computation of shock train phenomena inside a gas dynamic flow passage is studied. The flow passage is of rectangular cross-section with a diverging angle of 1.3°. Reynolds averaged Navier-Stokes (RANS) equations wi
Publikováno v:
Journal of Fluids Engineering. 140
Present investigation deals with the interaction of an incident oblique shock wave on a turbulent boundary layer over a wavy surface. The oblique shock wave was generated by an 8 deg wedge in a freestream Mach number of 2.0. Three-dimensional (3D) Re
Autor:
Shigeru Matsuo, Yuichi Mitsutake, Saeedur Rahman, A. B. M. Toufique Hasan, Md. Saddam Hossain Joy, Toshiaki Setoguchi
Publikováno v:
AIP Conference Proceedings.
A numerical computation was performed of an oblique shock wave impinging on turbulent boundary layer developing on a flat surface. The free stream flow was at M∞ = 2.0 with unit Reynolds number, Re = 10.5×106 m-1. A wedge having an angle of 8° wi
Autor:
Toshiaki Setoguchi, M. Ali, Shigeru Matsuo, A. B. M. Toufique Hasan, Saeedur Rahman, Md. Saddam Hossain Joy, Yuichi Mitsutake
Publikováno v:
AIP Conference Proceedings.
A numerical computation of an oblique shock wave incident on a turbulent boundary layer was performed for free stream flow of air at M∞ = 2.0 and Re1 = 10.5×106 m−1. The oblique shock wave was generated from a 8° wedge. Reynolds averaged Navier