From b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b Mon Sep 17 00:00:00 2001 From: priyanka Date: Wed, 24 Jun 2015 15:03:17 +0530 Subject: initial commit / add all books --- 548/DEPENDENCIES/6_17data.sci | 17 +++++++++++++++++ 1 file changed, 17 insertions(+) create mode 100755 548/DEPENDENCIES/6_17data.sci (limited to '548/DEPENDENCIES/6_17data.sci') diff --git a/548/DEPENDENCIES/6_17data.sci b/548/DEPENDENCIES/6_17data.sci new file mode 100755 index 000000000..c44970687 --- /dev/null +++ b/548/DEPENDENCIES/6_17data.sci @@ -0,0 +1,17 @@ +//for the jet power executive aircraft(CJ-1): +W=88176.75;//normal gross weight(N) +b=16.25;//wingspan(meter) +S=29.54;//wingarea(m^2) +AR=b^2/S;//aspect ratio +e=0.81;//oswald efficiency factor +h=1.83;//Height(m)of wing above ground +D=1.225;//density at sea level(Kg/m^3) +g=9.8;//Gravitational constant +Ur=0.02;//Rolling friction coefficient +Cl=1.0;//maximum lift coefficient during ground roll +Cdo=0.02;//parasite drag coefficient +T=32485;//thrust(N) +phi=(16*h/b)^2/(1+(16*h/b)^2)//Ground effect factor +Vlo=1.2*sqrt(2*W/(D*S*Cl))//liftoff velocity(1.2*Vstall in m/s) +Dr=D*(0.7*Vlo)^2*S*(Cdo+phi*Cl^2/(%pi*e*AR))/2//drag(N) +L=D*(0.7*Vlo)^2*S*Cl/2//lift(N) -- cgit