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There were differences in thrust force produced by individual strokes within a particular powerstroking bout, and a trend for the thrust per stroke to decreases as the time spent swimming increased.
Differences in thrust per stoke may be caused by differences in stroke amplitude and/or differences in the angle of the flipper blade or even stiffness of the flipper as it moves through the water increased mean thrust coefficient, or increased acceleration reaction due to decreased duration of acceleration phases of stroke cycle.
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These observations have been noted previously (Booth, 2009; Ischer et al., 2009; Booth and Evans, 2011; Booth et al., 2013) but an explanation of the mechanism for difference in thrust produced per stroke had not been investigated.
We still need many more descriptions of shale-prone fault zones to understand the potential variations in thrust sheet structural style caused by differences in shale detachment characteristics.
The obtained results show that there are many differences in performance behaviors of the aerostatic thrust bearing caused by different orifice chamber shapes.
The aerodynamic design was focused on the minimization of the difference, in terms of thrust coefficient, with respect to the full scale reference.
Depth variation of differences in seismic magnitude differentials mb−Mw for interplate thrust events on the megathrusts along the Kuril, Sumba, Aleutians and Peru subduction zones.
Fig. 5. Depth variation of differences in seismic magnitude differentials mb−Mw for interplate thrust events on the megathrusts near the 2011 Tohoku, 2004 Sumatra, and 2010 Chile great earthquakes.
We will obtain preliminary estimates of variability and effect size to determine if differences in spinal manipulation delivery, as estimated by thrust contact force and spinal segment load, are related to patient-centered outcomes.
Balancing cross sections is an important technique in thrust belts.
Thrust generated early in the downstroke was most likely generated by lift-based thrust while drag-based thrust was most likely responsible for the peak in thrust production that occurred later in the downstroke.
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