Zobrazeno 1 - 10
of 10
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
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
Autor:
Hossain Joy, Md Saddam, Nall, Duncan L., Emon, Bashar, Ki Yun Lee, Barishman, Alexandra, Ahmed, Movviz, Rahman, Saeedur, Selvin, Paul R., Saif, M. Taher A.
Publikováno v:
Proceedings of the National Academy of Sciences of the United States of America; 12/26/2023, Vol. 120 Issue 52, p1-10, 21p
Publikováno v:
AIP Conference Proceedings; 2018, Vol. 1980 Issue 1, p1-7, 7p, 1 Diagram, 6 Graphs
Publikováno v:
Lab on a Chip; 9/21/2019, Vol. 19 Issue 18, p2951-2957, 7p
Publikováno v:
Lab on a Chip; 9/21/2019, Vol. 19 Issue 18, p3133-3139, 7p