Composite Strength Scaling Effect Using Progressive Degradation Model

Rehan, Abdul Qadeer; Grote, Karl‐H.

doi:10.1109/csie.2009.905

Cited by 2 publications

(1 citation statement)

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“…For flexible composite rotors, scaling of the material is highly nontrivial, especially for the prediction of material failure. The effects of specimen size, material properties, stacking sequence, number of plies, and fiber orientation, among other characteristics, have been shown to have a significant effect on the failure strength of composite materials, as well as the failure mode of the test specimen [28][29][30][31][32][33].…”

Section: International Journal Of Rotating Machinerymentioning

confidence: 99%

Scaling of the Transient Hydroelastic Response and Failure Mechanisms of Self-Adaptive Composite Marine Propellers

Motley

Young

2012

International Journal of Rotating Machinery

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The load dependent deformation responses and complex failure mechanisms of self-adaptive composite propeller blades make the design, analysis, and scaling of these structures nontrivial. The objective of this work is to investigate and verify the dynamic similarity relationships for the hydroelastic response and potential failure mechanisms of self-adaptive composite marine propellers. A fully coupled, three-dimensional boundary element method-finite element method is used to compare the model and full-scale responses of a self-adaptive composite propeller. The effects of spatially varying inflow, transient sheet cavitation, and load-dependent blade deformation are considered. Three types of scaling are discussed: Reynolds scale, Froude scale, and Mach scale. The results show that Mach scaling, which requires the model inflow speed to be the same as the full scale, will lead to discrepancies in the spatial load distributions at low speeds due to differences in Froude number, but the differences between model and full-scale results become negligible at high speeds. Thus, Mach scaling is recommended for a composite marine propeller because it allows the same material and layering scheme to be used between the model and the full scale, leading to similar 3D stress distributions, and hence similar failure mechanisms, between the model and the full scale.

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