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Diffstat (limited to '548/DEPENDENCIES/2_1data.sci')
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diff --git a/548/DEPENDENCIES/2_1data.sci b/548/DEPENDENCIES/2_1data.sci new file mode 100755 index 000000000..f13cf2da6 --- /dev/null +++ b/548/DEPENDENCIES/2_1data.sci @@ -0,0 +1,5 @@ +//example 2.1: The air pressure and density at a point on the wing of a Boeing 747 are 1.10 * 10^5 N/m^2 and 1.20kg/m^3,respectively.what is temperature at that point?
+p=1.10*10^5;//given
+density=1.20;//given
+R=287;// gas constant.for air(j/kg.k)
+T=p/((density)*(R))
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