Takenori Maeda, Vijayan Baburaj, Tatsuzo Koga
Optical Engineering, Vol. 36, Issue 07, (July 1997) https://doi.org/10.1117/1.601401
TOPICS: Fiber reinforced polymers, Composites, Holographic interferometry, Fringe analysis, Shape analysis, Optical engineering, Laser interferometry, Holography, Nondestructive evaluation, Finite element methods
A test method for the evaluation of the in-plane shear modulus of composite laminates is presented. The method is essentially a resonance test on a cantilevered rectangular orthotropic laminate using laser holographic interferometry. Based on Rayleigh’s quotient, a simple formula is derived to determine the in-plane shear modulus using the resonance frequency of the first torsional vibration. An appropriate value of the length-to-width (aspect) ratio of the specimen is suggested to evaluate the in-plane shear modulus accurately. The results show that the measured in-plane shear moduli by the present method agree well with the modulus obtained by a ±45-deg off-axis tensile test.