yc90
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can anyone explain to me wad is the angle of projection of a projectile motion for the longest range with wind resistance?
The optimal angle of projection for achieving the longest range of a projectile under wind resistance conditions is not fixed at 45 degrees, as it is in the absence of air resistance. The angle must be adjusted based on the magnitude of wind resistance, with increased resistance necessitating a lower angle for maximum distance. The discussion outlines the equations of motion for both the X and Y axes, incorporating air resistance as a variable affecting projectile motion. The final equations derived include y = -g*t/B + Vo*Sin(θ)*t*e^(B*t) and x = Vo*Cos(θ)*t*e^(-B*t), which can be used to analyze projectile trajectories under varying conditions.
PREREQUISITESThis discussion is beneficial for physicists, engineers, and students studying mechanics, particularly those interested in optimizing projectile motion in the presence of air resistance.
x = Vo*Cos(θ)*t
y = Vo*Sin(θ)*t + .5*g*t^2
t = 2*Vo*Sin(θ)/g
x = 2*Vo^2*Cos(θ)*Sin(θ)/g
x' = (2 * Vo^2)(cos^2(θ) - Sin^2(θ))
x' = (2 * Vo^2)(1 - 2 * Sin^2(θ))
0 = (1 - 2 * Sin^2(θ))
θ = 45 degrees
F = α * v
a = α * v / m
a = Β * v
d2y/dt2 = g + Β*dy/dt
d2y/dt2 - Β*dy/dt = g
y = C1 *e^(Βt) + C2*t*e^(Βt)
y(0) = 0
y'(0) = Vo*Sin(θ)
0 = C1 *e^(Β*0) + C2*0*e^(Β*0)
C1 = 0
y = C2*t*e^(Βt)
y' = C2*(t*Β*e^(Β*t) + e^(Βt))
C2 = Vo*Sin(θ)
Yh = Vo*Cos(θ)*t*e^(Β*t)
d2y/dt2 - Β*dy/dt = g
Yp = A*t
Yp' = A
Yp'' = 0
d2y/dt2 - Β*dy/dt = g
0 - Β*A = g
A = -g/Β
Yp = -g*t/B
y = Yp + Yh
[B]y = -g*t/B + Vo*Sin(θ)*t*e^(B*t)[/B]
d2x/dt2 = -Β*dx/dt
d2x/dt2 + Β*dx/dt= 0
x = C1 *e^(-Βt) + C2*t*e^(-Βt)
x(0) = 0
x'(0) = Vo*Cos(θ)
C1 = 0
C2 = Vo*Cos(θ)
x = Vo*Cos(θ)*t*e^(-B*t)
[B][SIZE="4"]y = -g*t/B + Vo*Sin(θ)*t*e^(B*t)
x = Vo*Cos(θ)*t*e^(-B*t)[/B]
0 = -g*t/B + Vo*Sin(θ)*t*e^(B*t)
t = ln(g/(B*Vo*Sin(θ)))/B
x = Vo * Cos(θ) * ln(g/(B*Vo*Sin(θ)))/B * e^(-ln(g/(B*Vo*Sin(θ))))
x' = -((e^-ln[(g Csc[θ])/(B*Vo)]*Vo*Cos[θ]*Cot[θ])/B) + (e^-ln[(g Csc[θ])/(B*Vo)]*Vo*Cos[θ]*Cot[θ]*ln[e]*ln[(g*Csc[θ])/(B*Vo)])/B - (e^-ln[(g Csc[θ])/(B*Vo)]*Vo*ln[(g*Csc[θ])/(B*Vo)]*Sin[θ])/B
0 = Cos[θ]*Cot[θ] + Cos[θ]*Cot[θ]*ln[(g*Csc[θ])/(B*Vo)]) - ln[(g*Csc[θ])/(B*Vo)]*Sin[θ]
Thats interesting, I never knew that :)lzkelley said:The force of air resistance starts out approximately linearly (as swraman used), and is a good approx for small-medium object at low-medium speeds. For larger objects and higher speeds the resistance goes approximately as a (~)square of the velocity (i totally can't remember the details by i think the exact value of the exponent varies with the shape of the object??), and finally begins to level out asymptotically (this comes from fluid approximations where a fairly large enveloped develops around the projectile shielding it from air resistance).