Exact(8)
The results show that the deflection is still in the acceptable range.
We show that the deflection during rotation is directly proportional to the sample viscosity.
The tested results from LDV show that the deflection of the piezoelectric cantilever is linear with the driving voltage.
The computational results show that the deflection arising from gravity of the moving components may have significant influence on the pose accuracy of the end-effector.
The results show that the deflection distribution does not tend toward the planar flame solution with increasing radius as might have been expected.
The experiments of the stiffness and rotation error of the spindle show that the deflection of the shaft resulting from the calculating parameters in the micro scale is very close to the deviation of the spindle system.
We show that the deflection of neutral hydrogen flow from its original direction in the unperturbed LISM is highly anisotropic and evaluate a possible angle between the hydrogen deflection plane measured in the SOHO SWAN experiment and the plane containing the ISMF and LISM velocity vectors for different ISMF strengths.
The results show that the deflection of G1 at the center span was less than that of G2 due to the load being applied onto G2.
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