Sentence examples for blade were calculated from inspiring English sources

The aerodynamic forces of the rotor blade were calculated using two-dimensional quasi-steady strip theory.

Utilising this method, the modal damping parameters of the compressor blade were calculated based on direction-dependent material properties of single unidirectional carbon fibre-reinforced epoxy layers.

The head extension and LBLM angles with each laryngoscope blade were calculated and compared with the paired t-test.

The force of each element on the blade is calculated by the unsteady Bernoulli equation.

The probability of failure in flapwise bending of the rotor blade is calculated by means of a first-order reliability method, and contributions to this probability from all local maxima of the load response process over the operational life are integrated.

When the average ratio of BrdU labeling in the suprapyramidal to infrapyramidal blade was calculated, a ratio of 1.75 of suprapyramidal to infrapyramidal BrdU labeling was significantly reduced to a ratio of 0.91 following 13- cis RA treatment (Fig. 4C).

Discretized by the Galerkin approximation, eigenvalues and vectors and nonlinear steady state static response of the nanocomposite beams and blades were calculated.

The aerodynamic loading on the blades are calculated using a quasi-steady modeling.

Furthermore, local angle of attack and net incident velocity on the blades are calculated from the local velocity field.

The normal and tangential drag forces on each blade of the Savonius rotor model were calculated using the measured pressure difference between the concave and convex surfaces of the blades using Equations 9 and 10. Figure 3 shows the cross section of the rotor with the normal and tangential drag force directions.

The total root mean square displacements of a curved thin blade subjected to turbulent boundary layers were calculated and illustrated as a function of free stream velocity and damping ratio.