Projectile launched from a cannon at an elevation angle of and velocity vl.
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As you described, we substitute y=0y=0and x=Rx=R into the trajectory equation:
0=H+Rtanθ−R2g2u2sec2θ.(1)(1)0=H+Rtanθ−R2g2u2sec2θ.
Then, differentiating with respect to θθ and setting dRdθ=0dRdθ=0:
0=Rmaxsec2θ−R2maxg2u22sec2θtanθ,0=Rmaxsec2θ−Rmax2g2u22sec2θtanθ,
which simplifies to
Rmax=u2gcotθ.(2)(2)Rmax=u2gcotθ.
Solving (1)(1) and (2)(2) will yield the desired expressions for θθ and RmaxRmax.
0=H+Rtanθ−R2g2u2sec2θ.(1)(1)0=H+Rtanθ−R2g2u2sec2θ.
Then, differentiating with respect to θθ and setting dRdθ=0dRdθ=0:
0=Rmaxsec2θ−R2maxg2u22sec2θtanθ,0=Rmaxsec2θ−Rmax2g2u22sec2θtanθ,
which simplifies to
Rmax=u2gcotθ.(2)(2)Rmax=u2gcotθ.
Solving (1)(1) and (2)(2) will yield the desired expressions for θθ and RmaxRmax.
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