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authorpriyanka2015-06-24 15:03:17 +0530
committerpriyanka2015-06-24 15:03:17 +0530
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initial commit / add all books
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+H=2000;//standard altitude at which airplane is flying(meter)
+P=7.95*10^4;//pressure corresponding to standard altitude,N/m^2
+D=1.0066;//density corresponding to standard altitude,Kg/m^3
+P1=7.58*10^4;//pressure at a point on wing,N/m^2
+V=70;//airplane velocity in m/s
+q=D*V^2/2 //dynamic pressure,N/m^2