A Numerical Study of Aerodynamic Force Generation Mechanism for 2-D Insect Wing Motion

2006 ◽  
Author(s):  
Jung Sang Lee ◽  
Chongam Kim
Keyword(s):  
Aerodynamic Force ◽  
Numerical Study ◽  
Generation Mechanism ◽  
Force Generation ◽  
Insect Wing ◽  
Wing Motion

Numerical Study on the Unsteady-Force-Generation Mechanism of Insect Flapping Motion

AIAA Journal ◽  
2008 ◽  
Vol 46 (7) ◽  
pp. 1835-1848 ◽  
Author(s):  
Jung-Sang Lee ◽  
Jin-Ho Kim ◽  
Chongam Kim
Keyword(s):  
Numerical Study ◽  
Generation Mechanism ◽  
Force Generation ◽  
Flapping Motion ◽  
Unsteady Force

Unsteady aerodynamic force generation by a model fruit fly wing in flapping motion

2002 ◽  
Vol 205 (1) ◽  
pp. 55-70 ◽  
Author(s):  
Mao Sun ◽  
Jian Tang
Keyword(s):  
Aerodynamic Force ◽  
Lift Coefficient ◽  
Unsteady Aerodynamics ◽  
Fruit Fly ◽  
Force Generation ◽  
Generation Process ◽  
Flapping Motion ◽  
Unsteady Aerodynamic ◽  
The Mean ◽  
Unsteady Aerodynamic Force

SUMMARY A computational fluid-dynamic analysis was conducted to study the unsteady aerodynamics of a model fruit fly wing. The wing performs an idealized flapping motion that emulates the wing motion of a fruit fly in normal hovering flight. The Navier–Stokes equations are solved numerically. The solution provides the flow and pressure fields, from which the aerodynamic forces and vorticity wake structure are obtained. Insights into the unsteady aerodynamic force generation process are gained from the force and flow-structure information. Considerable lift can be produced when the majority of the wing rotation is conducted near the end of a stroke or wing rotation precedes stroke reversal (rotation advanced), and the mean lift coefficient can be more than twice the quasi-steady value. Three mechanisms are responsible for the large lift: the rapid acceleration of the wing at the beginning of a stroke, the absence of stall during the stroke and the fast pitching-up rotation of the wing near the end of the stroke. When half the wing rotation is conducted near the end of a stroke and half at the beginning of the next stroke (symmetrical rotation), the lift at the beginning and near the end of a stroke becomes smaller because the effects of the first and third mechanisms above are reduced. The mean lift coefficient is smaller than that of the rotation-advanced case, but is still 80 % larger than the quasi-steady value. When the majority of the rotation is delayed until the beginning of the next stroke (rotation delayed), the lift at the beginning and near the end of a stroke becomes very small or even negative because the effect of the first mechanism above is cancelled and the third mechanism does not apply in this case. The mean lift coefficient is much smaller than in the other two cases.

Experimental and Numerical Study on the Flow Field Around a Parallel-Foil Turbine

2020 ◽  
Author(s):  
Yulu Wang ◽  
Di Zhang ◽  
Yonghui Xie
Keyword(s):  
Flow Field ◽  
Aerodynamic Force ◽  
Numerical Study ◽  
Energy Extraction ◽  
Reduced Frequency ◽  
Image Velocimetry ◽  
Efficiency Increase ◽  
Oscillation Process ◽  
Effective Angle ◽  
Extraction Performance

Abstract An experiment facility of parallel-foil turbine is proposed in this study. The flow field around foils at different reduced frequency, pitching amplitude and plunging amplitude is measured by 2D Particle Image Velocimetry (PIV) system. And the energy extraction performance at different motion parameters is analyzed numerically. The comparison between experimental and numerical flow field is conducted at different reduced frequency. The evolution of flow field and the aerodynamic force with different pitching amplitude and plunging amplitude are discussed. The effect of pitching amplitude and plunging amplitude on energy extraction performance is obtained. Results indicate that the pitching amplitude can increase the range and the strength of acceleration area by varying the pitching velocity and the effective angle of attack. The optimal extraction performance appears at 70°. Due to the increase in plunging amplitude, the energy extraction performance and efficiency increase gradually. The optimal plunging amplitude is 1.0. The pitching amplitude and the plunging amplitude influence the power output by affecting the vortex shedding and the flow reattachment in oscillation process.

scholarly journals A chordwise offset of the wing-pitch axis enhances rotational aerodynamic forces on insect wings: a numerical study

2019 ◽  
Vol 16 (155) ◽  
pp. 20190118 ◽  
Author(s):  
Wouter G. van Veen ◽  
Johan L. van Leeuwen ◽  
Florian T. Muijres
Keyword(s):  
Flight Control ◽  
Numerical Study ◽  
Force Production ◽  
Aerodynamic Forces ◽  
Rotational Force ◽  
Wing Motion ◽  
Forward Stroke ◽  
Insect Wings ◽  
Force Mechanism ◽  
Numerical Parametric Study

Most flying animals produce aerodynamic forces by flapping their wings back and forth with a complex wingbeat pattern. The fluid dynamics that underlies this motion has been divided into separate aerodynamic mechanisms of which rotational lift, that results from fast wing pitch rotations, is particularly important for flight control and manoeuvrability. This rotational force mechanism has been modelled using Kutta–Joukowski theory, which combines the forward stroke motion of the wing with the fast pitch motion to compute forces. Recent studies, however, suggest that hovering insects can produce rotational forces at stroke reversal, without a forward motion of the wing. We have conducted a broad numerical parametric study over a range of wing morphologies and wing kinematics to show that rotational force production depends on two mechanisms: (i) conventional Kutta–Joukowski-based rotational forces and (ii) a rotational force mechanism that enables insects with an offset of the pitch axis relative to the wing's chordwise symmetry axis to generate rotational forces in the absence of forward wing motion. Because flying animals produce control actions frequently near stroke reversal, this pitch-axis-offset dependent aerodynamic mechanism may be particularly important for understanding control and manoeuvrability in natural flyers.

Numerical Analysis on Aerodynamic Force Generation of Biplane Counter-Flapping Flexible Airfoils

2009 ◽  
Vol 46 (5) ◽  
pp. 1785-1794 ◽  
Author(s):  
Jr-Ming Miao ◽  
Wei-Hsin Sun ◽  
Chang-Hsien Tai
Keyword(s):  
Numerical Analysis ◽  
Aerodynamic Force ◽  
Force Generation ◽  
Flexible Airfoils

Numerical Study on Pressure Generation Mechanism of Oil Film under Oil Control Ring

2019 ◽  
Author(s):  
Susumu Degawa ◽  
Wataru Kobayashi ◽  
Koji Kikuhara ◽  
Koichi Nishibe ◽  
Akemi Ito
Keyword(s):  
Numerical Study ◽  
Generation Mechanism ◽  
Oil Film
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