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The maximum average velocity reduction ratio reaches around 25%, when the row spacing reduces to zero, and the baffles lose their deceleration ability when the row spacing increases to 1.42 m and the velocity reduction ratio is − 13%.
A maximum average velocity of 65.4 ± 8.5 μm·s–1 is achieved near the platinum silicon boundary.
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It has been experimentally shown that the proposed design can levitate 1 mm × 1 mm sized and 7 μm thick micro-objects to a maximum height of 75 μm and propel them forward continuously at a maximum average forward velocity of 3.6 mm/s.
Half times and maximum or average velocities for furrow ingression and spindle pole separation were calculated from the regression lines with Mathematica software (Wolfram Research).
The maximum average flame propagation velocities of 0.5%, 1.2%, and 2.3% mixtures were 6.22 m/s, 8.31 m/s, and 12.91 m/s respectively.
It has analysed ANOVA F-test correlated to experimental SSR data verified and can set to critical value into SSR range between 0.3 to 0.4 values of average velocity or maximum point range of average velocity 0.4 mm/h.
A novice driver drives the vehicle 9.18 km/h (average velocity) and the maximum velocity is 12.72 km/h.
Each of these segments is verified with respect to its conformance with the average velocity and the maximum allowed speed on the respective road segments.
In the vicinity of the platinum silicon border, the average velocity reaches its maximum value, 12.0 ± 2.5 μm·s–1.
Therefore: :v_{av}=\frac{d}{\Delta t}=\frac{0.57}{4.5\times10^{-3}}=127\Thet {cm/s} The velocity of the wings is zero both at the beginning and at the end of the wing stroke, meaning the maximum linear velocity is higher than the average velocity.
The maximum measured velocity was approximately 1.61 times the average velocity.
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