Natural Frequency Calculator
The natural frequency is the rate at which a system oscillates autonomously.The formula is given by: Where: k is the stiffness of the system. m is the mass of the system.
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The natural frequency is the rate at which a system oscillates autonomously.The formula is given by: Where: k is the stiffness of the system. m is the mass of the system.
Natural Frequency Calculator Read More »
The modal damping equation relates the damping ratio to system parameters.The formula is given by: Where: ξ represents the modal damping ratio, c is the damping coefficient, m is the mass of the system, K is the stiffness of the system.
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Distance from axis with same moment of inertia mass.The formula is given by: Where: k is the radius of gyration, I is the moment of inertia of the object about the axis of rotation, and m is the mass of the object.
Radius of Gyration Equation Calculator Read More »
The modal stiffness equation defines the stiffness of a structure.The formula is given by: Where: Km = Modal stiffness m = Mass of the structure or system ω = Angular frequency of the mode of vibration
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Material failure predicted by comparing strain energy to critical limit.The formula is given by: Where: U is the strain energy density, σ is the stress applied to the material, ϵ is the corresponding strain.
Strain Energy Density Theory Calculator Read More »
Critical load causing structural instability in elastic columns predicted mathematically.The formula is given by: Where: P is the critical buckling load, E is the modulus of elasticity of the material, I is the moment of inertia of the cross-sectional area of the column, k is the effective length factor (depends on the end conditions of the
Buckling Equation Calculator Read More »
Thin plate behavior analyzed, accounting for transverse shear deformation.The formula is given by: Where: D is the flexural rigidity of the plate. ∇⁴ is the biharmonic operator. w is the deflection of the plate. q(x,y) is the applied transverse load per unit area.
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Plate theory extending Euler-Bernoulli’s for thick plates analysis.The formula is given by: Where: D is the flexural rigidity of the plate. ∇⁴ is the biharmonic operator. w is the deflection of the plate. q is the applied transverse load.
Timoshenko’s Plate Theory Calculator Read More »
Graphical method for visualizing stress components in materials analysis.The formula is given by: Where: σx and σy are the normal stresses in the x and y directions, respectively. τxy is the shear stress acting on the xy-plane.
Mohr’s Circle Calculator Read More »
Material failure predicted when maximum stress exceeds critical value.The formula is given by: Where: σ₁ is the maximum principal stress σ_x is the normal stress in the x-direction σ_y is the normal stress in the y-direction
Maximum Principal Stress Theory Calculator Read More »