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From the experimental results, it was found that the designed blade had structural integrity.
It verifies that the optimum designed blade from the BEM was reliable.
As the mission requirements of the aero engine improve, the blade aerodynamic loadingis higher, especially for lightweight designed blade.
As the mission requirements of the aero engine improve, the blade aerodynamic loading is higher, especially for lightweight designed blade.
The tests are carried out using a designed blade tip section with applying standard lightning impulse voltages.
Numerical analysis results show that the designed blade structure was safe, and the value of stress and strain was low.
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Their common features include specially designed blades and the video cameras, integrated into the GlideScope blade or as external accessory attached onto the Airtraq Laryngoscope, which provide better laryngeal views [ 3, 4].
BEM analysis, however, shows that designing blades with proper twist and pitch angles, and targeting suitable TSR could lead to substantial gain (over 10%) in the performance.
There are three principal methods for designing blades: circular arc method, point-by-point method, and conformal representation.
The code illustrated these effects and results show designing blades with proper twist angle that harmonized with suitable TSR and pitch angle can definitely lead to substantial gain in performance of over 10%.
To attain a large steady loading on the stability boundary of the first mode bending vibration, it is advantageous to design blades with the angle of attack decreasing and the chamber and thickness increasing from hub to tip.
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