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Diffstat (limited to '1325/CH2/EX2.13/ex2_13.sce')
-rw-r--r-- | 1325/CH2/EX2.13/ex2_13.sce | 22 |
1 files changed, 22 insertions, 0 deletions
diff --git a/1325/CH2/EX2.13/ex2_13.sce b/1325/CH2/EX2.13/ex2_13.sce new file mode 100644 index 000000000..3e764705d --- /dev/null +++ b/1325/CH2/EX2.13/ex2_13.sce @@ -0,0 +1,22 @@ +//to find the gyroscopic reaction of the airscrew on the aeroplane when it has a) three blades and b)two blades
+//gravitaional force (g)=32.2 ft/s^2
+clc
+//given
+printf("\n")
+I=250//lb ft2
+n=1600//rpm
+v=150//mph
+r=500//ft
+w=%pi*160/3//angular velocity of rotation
+wp=(150*88)/(60*500)//angular velocity of precession
+//a) with three bladed screw
+//T=I*w*wp
+T=(250/32.2)*%pi*(160/3)*wp
+//b)with two bladed air screw
+//T1=2*I*w*wp*sin(o)
+printf("The magnitude of gyroscopic couple is given by %.0f lb ft\n",T)
+//Tix=T(1-cos(2o)) lb ft
+//T1y=Tsin(2o)) lb ft
+printf("The component gyroscopic couple in the vertical plane =%.0f(1-cos(2x)) lb ft\n",T)
+printf("The component gyroscopic couple in the horizontal plane =%.0f(sin(2x)) lb ft\n",T)
+// for direction refer the book example
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