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Materials Engineering (Non-Linear Fractional Material Strain) Solution

Problem Overview

We calculate the absolute rate dvdT\frac{dv}{dT} and fractional rate of thermal expansion 1vdvdT\frac{1}{v}\frac{dv}{dT} for an aerodynamic polymer composite governed by:

v(T)=(T2+1)ln⁑(T)v(T) = (T^2 + 1)^{\ln(T)}
evaluated at the temperature baseline T=eT = e.


Step-by-Step Mathematical Solution

Step 1: Formally Apply Logarithmic Differentiation

The governing process is Logarithmic Differentiation:

ln⁑v=ln⁑[(T2+1)ln⁑T]\ln v = \ln\left[ (T^2 + 1)^{\ln T} \right]
(This technique is defined in Logarithmic Differentiation.)

Bring the variable exponent down using the Power Property of logarithms:

ln⁑v=ln⁑(T)β‹…ln⁑(T2+1)\ln v = \ln(T) \cdot \ln(T^2 + 1)

Step 2: Differentiate Both Sides with Respect to Temperature TT

Apply the Product Rule on the right side with u=ln⁑(T)u = \ln(T) and w=ln⁑(T2+1)w = \ln(T^2 + 1):

ddT[ln⁑v]=ddT[ln⁑T]β‹…ln⁑(T2+1)+ln⁑(T)β‹…ddT[ln⁑(T2+1)]\frac{d}{dT}[\ln v] = \frac{d}{dT}[\ln T] \cdot \ln(T^2 + 1) + \ln(T) \cdot \frac{d}{dT}[\ln(T^2 + 1)]
1vdvdT=(1T)β‹…ln⁑(T2+1)+ln⁑(T)β‹…(2TT2+1)\frac{1}{v}\frac{dv}{dT} = \left(\frac{1}{T}\right) \cdot \ln(T^2 + 1) + \ln(T) \cdot \left(\frac{2T}{T^2 + 1}\right)
1vdvdT=ln⁑(T2+1)T+2Tln⁑TT2+1\frac{1}{v}\frac{dv}{dT} = \frac{\ln(T^2 + 1)}{T} + \frac{2T \ln T}{T^2 + 1}

Step 3: Identify the Fractional Rate of Expansion

Because the problem specifically asks for the fractional rate 1vdvdT\frac{1}{v}\frac{dv}{dT}, we do not need to multiply by vv:

Fractional Rate=1vdvdT=ln⁑(T2+1)T+2Tln⁑TT2+1\text{Fractional Rate} = \frac{1}{v}\frac{dv}{dT} = \frac{\ln(T^2 + 1)}{T} + \frac{2T \ln T}{T^2 + 1}

Step 4: Evaluate at T=eT = e

Recall that ln⁑(e)=1\ln(e) = 1:

1vdvdT∣T=e=ln⁑(e2+1)e+2eln⁑(e)e2+1=ln⁑(e2+1)e+2ee2+1\left.\frac{1}{v}\frac{dv}{dT}\right|_{T=e} = \frac{\ln(e^2 + 1)}{e} + \frac{2e \ln(e)}{e^2 + 1} = \frac{\ln(e^2 + 1)}{e} + \frac{2e}{e^2 + 1}
Numerically, since eβ‰ˆ2.71828e \approx 2.71828 and e2+1β‰ˆ8.389e^2 + 1 \approx 8.389:
ln⁑(8.389)β‰ˆ2.1269β€…β€ŠβŸΉβ€…β€Š2.12692.7183+5.43668.389β‰ˆ0.7824+0.6481β‰ˆ1.4305Β unitsβˆ’1\ln(8.389) \approx 2.1269 \implies \frac{2.1269}{2.7183} + \frac{5.4366}{8.389} \approx 0.7824 + 0.6481 \approx 1.4305\text{ units}^{-1}


Engineering Conclusion

At T=eT = e, the fractional volumetric expansion rate of the composite material is β‰ˆ1.43Β Kβˆ’1\approx 1.43\text{ K}^{-1} (meaning volume expands by approximately 143%143\% per normalized temperature unit). In aerospace and materials engineering, capturing the logarithmic derivative directly yields the linear/volumetric coefficient of thermal expansion (CTE) without requiring cumbersome multiplication by the base volume function v(T)v(T). This enables stress engineers to predict thermal delamination thresholds along aircraft radome seams during high-speed atmospheric cruise.