scholarly journals Inter-day session reliability of a novel assessment for rotational power of the pelvis, spine and trunk

2017 ◽  
Vol 1 (2) ◽  
Author(s):  
Thomas G. Palmer
Keyword(s):  
1980 ◽  
Vol 16 (5) ◽  
pp. 1218-1220 ◽  
Author(s):  
A. Cecchetti ◽  
F. Masoli ◽  
M. Poppi ◽  
G. Soardo

2012 ◽  
Vol 26 (3) ◽  
pp. 720-724 ◽  
Author(s):  
Matthew J Andre ◽  
Andrew C Fry ◽  
Melissa A Heyrman ◽  
Andrea Hudy ◽  
Brady Holt ◽  
...  

2007 ◽  
Vol 591 ◽  
pp. 321-337 ◽  
Author(s):  
ATTILA J. BERGOU ◽  
SHENG XU ◽  
Z. JANE WANG

Wing pitch reversal, the rapid change of angle of attack near stroke transition, represents a difference between hovering with flapping wings and with a continuously rotating blade (e.g. helicopter flight). Although insects have the musculature to control the wing pitch during flight, we show here that aerodynamic and wing inertia forces are sufficient to pitch the wing without the aid of the muscles. We study the passive nature of wing pitching in several observed wing kinematics, including the wing motion of a tethered dragonfly, Libellula pulchella, hovering fruitfly, hovering hawkmoth and simplified dragonfly hovering kinematics. To determine whether the pitching is passive, we calculate rotational power about the torsion axis owing to aerodynamic and wing inertial forces. This is done using both direct numerical simulations and quasi-steady fluid force models. We find that, in all the cases studied here, the net rotational power is negative, signifying that the fluid force assists rather than resists the wing pitching. To further understand the generality of these results, we use the quasi-steady force model to analyse the effect of the components of the fluid forces at pitch reversal, and predict the conditions under which the wing pitch reversal is passive. These results suggest the pitching motion of the wings can be passive in insect flight.


1974 ◽  
Vol 96 (1) ◽  
pp. 141-144
Author(s):  
M. A. M. A. Younes ◽  
F. R. Mobbs ◽  
J. E. R. Coney

The presence of secondary vortex motions in the flow between eccentric rotating cylinders is shown to increase the power input requirements to the inner rotating cylinder at any eccentricity ratio. The effect of superimposing axial flow is to delay the onset of instability and hence decrease this power input to the system. An evaluation of the rotational power losses due to instability as compared with the pumping power required to introduce the necessary axial flow rates is carried out for three gap-radius ratios.


1992 ◽  
Vol 112 (1-3) ◽  
pp. 91-94 ◽  
Author(s):  
J. Sievert ◽  
H. Ahlers ◽  
M. Enokizono ◽  
S. Kauke ◽  
L. Rahf ◽  
...  

Sign in / Sign up

Export Citation Format

Share Document