My Bedford and Fowler textbook (4th edition) has a chapter on numerical solutions. I'm having trouble understanding how the textbook splits up the components of force in the x and y directions to model the drag on a projectile:
The aerodynamic frag force on the projectile is of magnitude C|v2|, where C is a constant.
We must determine the x and y components of the total force on the projectile. Let D be the drag force. Because v/|v| is a unit vector in the direction of v, we can write the drag force as:
D=−C|v|2v|v|=C|v|v.
The external forces on the projectile are its weight and the drag so we have:
∑F=−mgj−C|v|v,
and the total components of the force are:
∑Fx=C√v2x+v2yvx
∑Fy=−mg−C√v2x+v2yvy.
I don't understand how the individual components of the drag force D=C|v|2 (acting in opposition to the projectile's movement) becomes something like this: −C√v2x+v2y∗vx ?
I understand that the absolute value of something can be represented as: |a|=√a2.
And the magnitude of velocity from its x and y components can be calculated as V=√v2x+v2y.
But I don't get how the non-absolute v term magically becomes vx or vy while the absolute term doesn't become |vx| or |vy| too.
What about equations without absolute values in them like the drag force equation? FD=12pv2ACD, where p,A,CD are constants. Would the horizontal and vertical components of forces then be:
Fx=−12pv2xACD
Answer
I find this type of question is always easier if you draw a diagram. The drag force F acts in the opposite direction to the velocity so it looks like:
and the components of the drag force are:
Fx=FcosθFy=Fsinθ
cosθ is vx/v and v=√v2x+v2y so we get:
Fx=Fvx√v2x+v2y
Since F=−Cv2 we get:
Fx=−Cv2vx√v2x+v2y
and because v=√v2x+v2y this becomes:
Fx=−C(v2x+v2y)vx√v2x+v2y=−Cvx√v2x+v2y
And likewise for Fy.
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