Multi-Disciplinary Computational Investigations on Asymmetrical Failure Factors of Disc Brakes for Various CFRP Materials: A Validated Approach

Finite element analyses (FEA) are flexible and advanced approaches, which utilized to address difficult problems of aerospace materials that exhibit both structural symmetrical asymmetrical characteristics. Frictional behavior effects used as a crucial in this multidisciplinary study, other structural, thermal properties computed using FEA. Primary lightweight such glass fiber reinforced polymer (GFRP), carbon (CFRP), kevlar (KFRP), titanium alloy, tungsten carbide, steel alloys, materials, silicon carbide (SiC) mixer, based on aforesaid underwent comprehensive investigations aircraft disc brake, two-wheeler ASTM general rotating test specimen (G-99). Standard boundary conditions, computational sensitivity tests, theoretical validations were conducted because the working nature FEA may impair output dependability. First, calculations performed standard component with two separate material families at various rotational velocities 400 RPM, 500 600 800 10 N external frictional force. Via tribological experiments, force deformation outcomes validated; experimental serve important conditions for real-time simulations. Second, verified was extended complicated applications brakes automobile brakes. This work confirms composite possess superior conventional alloys vehicle