Side‐to‐side supermicrosurgical anastomosis training using chicken wing model with V‐shaped traction method

Microsurgery ◽  
2021 ◽  
Author(s):  
Dewi Aisiyah Mukarramah ◽  
Reiko Tsukuura ◽  
Takashi Kageyama ◽  
Hayahito Sakai ◽  
Yuma Fuse ◽  
...  
Keyword(s):  
Traction Method ◽  
Wing Model

Analysis of Drag for an Aircraft Wing Model with and without Winglet

2011 ◽  
Vol 1 (7) ◽  
pp. 89-91
Author(s):  
Mitul Patel ◽  
◽  
Sharvil Shah ◽  
Dharmendra Dubey
Keyword(s):  
Aircraft Wing ◽  
Wing Model

Oscillating aero-wing model in the quasi-steady domain

2007 ◽  
Vol 1 (2) ◽  
pp. 87-99
Author(s):  
P. Freymuth
Keyword(s):  
Wing Model

Experimental study of natural disturbances of a supersonic boundary layer on a swept-wing model with periodic roughness

2020 ◽  
Author(s):  
A. A. Yatskikh ◽  
A. V. Panina ◽  
Yu. G. Yermolaev ◽  
A. D. Kosinov ◽  
N. V. Semionov
Keyword(s):  
Boundary Layer ◽  
Experimental Study ◽  
Supersonic Boundary Layer ◽  
Natural Disturbances ◽  
Swept Wing ◽  
Wing Model

Effectiveness of a microsurgery training program using a chicken wing model

2021 ◽  
pp. 1-7
Author(s):  
Aniket Dave ◽  
Maneesh Singhal ◽  
Raja Tiwari ◽  
Shashank Chauhan ◽  
Moumita De
Keyword(s):  
Training Program ◽  
Wing Model

Numerical and Experimental Analysis of 3D Micro-Corrugated Wing in Gliding Flight

2021 ◽  
Author(s):  
Nasim Chitsaz ◽  
Kamran Siddiqui ◽  
Romeo Marian ◽  
Javaan S. Chahl
Keyword(s):  
Stokes Equations ◽  
Three Dimensional ◽  
Flow Characteristics ◽  
Aerodynamic Performance ◽  
Numerical Results ◽  
Three Dimensional Model ◽  
Wing Model ◽  
Computational Fluid Dynamics Analysis ◽  
Gliding Flight ◽  
Flat Profile

Abstract In this study, computational fluid dynamics analysis was performed on a three-dimensional model of a Libellulidae wing to determine aerodynamic performance in gliding flight. The wing is comprised of various corrugated features alongside the spanwise and chordwise directions, as well as twist. The detailed features of real 3D dragonfly wing models, including all the corrugations through both span and chord, have not been considered in the past for a detailed aerodynamic analysis. The simulations were conducted by solving the Navier-Stokes equations to demonstrate gliding performance over a range of angles of attack at low Reynolds numbers. The numerical model was validated against experimental data obtained from a fabricated corrugated wing model using particle image velocimetry. The numerical results demonstrate that bio-inspired wings with corrugations compared to flat profile wings generate more lift with lower drag, trapping the vortices in the valleys of wing corrugation leading to delayed flow separation and delayed stall. The experimental and numerical results demonstrate that the methodology presented in this study can be used to measure bio-inspired 3D wing flow characteristics, including the influence of complex corrugations on aerodynamic performance. These findings contribute to the advancement of knowledge required for designing an optimized bioinspired micro air vehicle.

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