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Materials Engineering (Non-Linear Fractional Material Strain)

A materials scientist is evaluating an advanced carbon-fiber reinforced polymer matrix designed for high-altitude aerodynamic radomes. Under intense aerodynamic friction and thermal load, the material's volumetric expansion vv responds to the normalized operating temperature TT according to an empirical power-tower equation:

v(T)=(T2+1)ln⁡(T)(T>1)v(T) = (T^2 + 1)^{\ln(T)} \qquad (T > 1)

  1. Apply logarithmic differentiation to derive an expression for the volumetric sensitivity rate dvdT\frac{dv}{dT}.
  2. Determine the fractional rate of thermal expansion (defined as 1vdvdT\frac{1}{v}\frac{dv}{dT}, measuring percent expansion per degree temperature rise).
  3. Evaluate the exact fractional rate of expansion 1vdvdT\frac{1}{v}\frac{dv}{dT} at the critical temperature baseline T=eT = e.