For air at standard atmospheric pressure the values of the
Chapter 1, Problem 1.69(choose chapter or problem)
For air at standard atmospheric pressure the values of the constants that appear in the Sutherland equation (Eq. 1.10) are \(C=1.458 \times 10^{-6} \mathrm{~kg} /\left(\mathrm{m} \cdot \mathrm{s} \cdot \mathrm{K}^{1 / 2}\right)\) and S = 110.4 K. Use these values to predict the viscosity of air at \(\mathrm{10~^\circ C}\) and \(\mathrm{90~^\circ C}\) and compare with values given in Table B.4 in Appendix B.
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