Resonance Vibration of Mistuned Bladed Discs in Stationary Operations [PDF]
A numerical model for the calculation of resonance stationary response of mistuned bladed disc is presented. The bladed disc model includes all important effects on a rotating system of the real geometry. The excitation forces were calculated by a code on the basis of two-dimensional compressible flow (to M < 0.8) for thin airfoil blades.
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A potential treatment for COVID-19 based on modal characteristics and dynamic responses analysis of 2019-nCoV. [PDF]
Yao M, Wang H.
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Vibration Analysis and Damping Effect of Blade-Hard Coating Composite Structure Based on Base Excitation. [PDF]
Wang J, Guo T, Liu W, Wang Z, Zhang Y.
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Experimental Investigation on a Bladed Disk with Traveling Wave Excitation. [PDF]
Carassale L, Rizzetto E.
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The vibration response mechanism of a blade disk rotor system under the coupling effects of cracks and aerodynamic forces. [PDF]
Yang J, Xie J, Wang T, Yang F, Chen J.
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Improving Aeroelastic Stability of Bladed Disks with Topologically Optimized Piezoelectric Materials and Intentionally Mistuned Shunt Capacitance. [PDF]
Liu X, Fan Y, Li L, Yu X.
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State-Space Model for Arrival Time Simulations and Methodology for Offline Blade Tip-Timing Software Characterization. [PDF]
Tocci T +4 more
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Nonlinear vibrations of mistuned bladed disk assemblies
Yüksek çevrim nedeniyle oluşan yorulma son yirmi yıldır üzerinde yoğun bir şekilde çalışılan bir konudur. Jet motorları üzerindeki etkisi, motor kayıplarına hatta can kayıplarına sebep olacak kadar fazladır. Yorulma ömrünün hesaplanması için mekanik titreşimler sonucu oluşan gerilmelerin bulunması gerekmektedir.
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Free Vibration Analysis of a Graphene-Reinforced Porous Composite Plate with Different Boundary Conditions. [PDF]
Pan HG +5 more
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A random optical parametric oscillator. [PDF]
Tovar P +4 more
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