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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.
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The aerodynamic forces of the rotor blade were calculated using two-dimensional quasi-steady strip theory.
The head extension and LBLM angles with each laryngoscope blade were calculated and compared with the paired t-test.
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).
Furthermore, local angle of attack and net incident velocity on the blades are calculated from the local velocity field.
Discretized by the Galerkin approximation, eigenvalues and vectors and nonlinear steady state static response of the nanocomposite beams and blades were calculated.
The circulation is calculated at each blade element using the Kutta-Joukowski law [6]: Γ = 1 2 V rel ⋅ C ⋅ C l α Open image in new window.
The blade can be solid or hollow; in the latter case, s is calculated to ensure that the allowable maximum strain is not exceeded.
The mess is calculated.
Having determined the length of the blades the blade profiles (twist angles and chord lengths) at ten selected sections along the blade can be calculated.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com