For many gases the temperature dependence of the heat capacity C, of can be described in terms of a cubic equation: C = a+bT+cT²+dT³ The following table gives the coefficients of the cubic equation for four gases. C is in joules/(g mol)(°C) and 7 is in °C. Gas a b C d SO₂ 38.91 2 3.904 x 10 -3.105 x 10-5 -9 8.606 x 101 SO3 48.50 9.188 × 10 2 -8.540 x 10-5 -9 32.40 x 10 02 29.10 1.158 × 10 2 N₂ 29.00 -0.6076 × 10-5 0.2199 x 10-0.5723 × 10-5 -9 1.311 x 10 -2.871 × 10-9 Calculate the heat capacity for each gas at temperatures ranging between 200 and 400°C at 20°C increments. To present the results, create an 11x5 matrix where the first column is the temperature, and the second through fifth columns are the heat capacities of SO₂, SO3, O2, and №2, respectively.
For many gases the temperature dependence of the heat capacity C, of can be described in terms of a cubic equation: C = a+bT+cT²+dT³ The following table gives the coefficients of the cubic equation for four gases. C is in joules/(g mol)(°C) and 7 is in °C. Gas a b C d SO₂ 38.91 2 3.904 x 10 -3.105 x 10-5 -9 8.606 x 101 SO3 48.50 9.188 × 10 2 -8.540 x 10-5 -9 32.40 x 10 02 29.10 1.158 × 10 2 N₂ 29.00 -0.6076 × 10-5 0.2199 x 10-0.5723 × 10-5 -9 1.311 x 10 -2.871 × 10-9 Calculate the heat capacity for each gas at temperatures ranging between 200 and 400°C at 20°C increments. To present the results, create an 11x5 matrix where the first column is the temperature, and the second through fifth columns are the heat capacities of SO₂, SO3, O2, and №2, respectively.
C++ for Engineers and Scientists
4th Edition
ISBN:9781133187844
Author:Bronson, Gary J.
Publisher:Bronson, Gary J.
Chapter1: Fundamentals Of C++ Programming
Section: Chapter Questions
Problem 2PP: (Conversion) An object’s polar moment of inertia, J, represents its resistance to twisting. For a...
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