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Effect of Temperature Changes on the Natural Frequencies of Composite Beams
Study 1: Free Vibration Analysis of Laminated Composite Beams under Thermal Effects
This study investigates the influence of temperature variation on the free vibration characteristics of laminated composite beams. The beams analysed are made from graphite epoxy material with rectangular cross-sections. Different stacking sequences are considered, typically ranging from four to eight layers, with each lamina having equal thickness. The beam dimensions remain constant while the material orientation varies to examine its influence on thermal sensitivity.
The researchers use an analytical approach based on classical laminated beam theory combined with Hamilton’s principle. Temperature changes are introduced as uniform thermal loads across the beam length, which generate thermal stresses due to constrained expansion. Natural frequencies are calculated by solving the governing differential equations derived from the energy method.
The key result shows a clear reduction in natural frequencies as temperature increases. This occurs because elevated temperatures reduce the effective stiffness of the composite material, particularly in the matrix-dominated directions. The relationship between temperature and frequency is found to be nonlinear, with sharper reductions observed at higher temperature ranges.
The conclusions highlight that stacking sequence plays a critical role in thermal vibration behaviour, with angle-ply laminates being more sensitive to temperature changes than cross-ply configurations. A major strength of this study is its strong theoretical foundation and parametric depth. However, a weakness is the absence of experimental validation, which limits the real-world applicability of the findings. Overall, the study provides a solid analytical benchmark for understanding thermal effects on composite beam vibrations.
Study 2: Experimental Investigation of Temperature Effects on Composite Beam Frequencies
This study focuses on experimentally measuring the impact of temperature variation on the natural frequencies of carbon fibre reinforced polymer composite beams. The beams are manufactured with six unidirectional layers and standard laboratory-scale dimensions. Material properties are obtained directly from manufacturer data and verified through testing.
The experimental method involves placing the composite beams inside a temperature-controlled environmental chamber. Modal testing is performed using an impact hammer and accelerometers while the temperature is gradually increased. Frequency response functions are recorded and analysed using modal analysis software.
The results demonstrate a consistent decrease in natural frequency with increasing temperature. The first bending mode shows the highest sensitivity, while higher modes are comparatively less affected. This behaviour is attributed to temperature-induced softening of the polymer matrix, which reduces the overall flexural rigidity of the beam.
The study confirms a near-linear relationship between temperature increase and frequency reduction within the tested range. The conclusions emphasise that temperature must be accounted for in vibration-based health monitoring systems, as frequency shifts may not always indicate damage.
The main strength of this study lies in its experimental validation, which strengthens confidence in the results. However, the limited temperature range and focus on a single laminate configuration reduce its generalisability. Despite this, the study is valuable for practical engineering applications where real operating conditions must be considered.