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The rocket shown below is held stationary by the horizontal force, F_(x) and the vertical force, F_(y) . The velocity and pressure of the exhaust
The rocket shown below is held stationary by the horizontal force,
F_(x)
and the vertical force,
F_(y)
. The velocity and pressure of the exhaust gas are
5000f(t)/(sec)
and 20 psia at the nozzle exit, which has a cross sectional area of
60in^(2)
. The exhaust mass flowrate is constant at
21lb(m)/(sec)
.\ Determine the value of the restraining force
F_(x)
. Assume the exhaust flow is essentially horizontal.
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