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author | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
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committer | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
commit | 7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 (patch) | |
tree | dbb9e3ddb5fc829e7c5c7e6be99b2c4ba356132c /3765/CH1/EX1.3/Ex1_3.sce | |
parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
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diff --git a/3765/CH1/EX1.3/Ex1_3.sce b/3765/CH1/EX1.3/Ex1_3.sce new file mode 100644 index 000000000..d1ce816a7 --- /dev/null +++ b/3765/CH1/EX1.3/Ex1_3.sce @@ -0,0 +1,17 @@ +clc +// Example 1.3.py +// Calculate the isothermal compressibility for air at a pressure of 0.5 atm. + +// Variable declaration +p = 0.5 // pressure (atm) +p_si = 0.5*101325 // pressure (N/m^2) +p_eng = 0.5*2116 // pressure (lb/ft^2) + +// Calculations +tau_atm = 1/p // isothermal compressibility in atm^-1 +tau_si = 1/p_si // isothermal compressibility in m^2/N +tau_eng = 1/p_eng // isothermal compressibility in ft^2/lb + +// Result +printf("\n Isothermal compressibility for air at %.1f atm is %.2f atm^-1 or %.2e m^2/N or %.2e ft^2/lb", p, tau_atm, tau_si, tau_eng) + |