One of the widely used correlations to describe the variation of the viscosity of gases is the power-law equation given by μ/μ0 = (T/T0)n, where μ0 and T0 are the reference viscosity and temperature, respectively. Using the power and Sutherland laws, examine the variation of the air viscosity for the temperature range 100°C (373 K) to 1000°C (1273 K). Plot your results to compare with values listed in Table A-22. Take the reference temperature as 0°C and n = 0.666 for the atmospheric air.
Table A-22:
Note: For ideal gases, the properties cp, k, μ, and Pr are independent of pressure. The properties ρ, v, and α at a pressure P (in atm) other than 1 atm are determined by multiplying the values of P at the given temperature by ρ and by dividing v and α by P.
Source: Data generated from the EES software developed by S. A. Klein and F. L. Alvarado. Original sources: Keenan, Chao, Keyes, Gas Tables, Wiley, 1984; Thermophysical Properties of Matter. Vol. 3: Thermal Conductivity, Y. S. Touloukian, P. E. Liley, S. C. Saxena, Vol. 11: Viscosity, Y. S. Touloukian, S. C. Saxena, and P. Hestermans, IFI/Plenum, NY, 1970, ISBN 0-306067020-8.
We need at least 10 more requests to produce the solution.
0 / 10 have requested this problem solution
The more requests, the faster the answer.