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| Teaching Since: | May 2017 |
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MCS,PHD
Argosy University/ Phoniex University/
Nov-2005 - Oct-2011
Professor
Phoniex University
Oct-2001 - Nov-2016
The rocket shown in Fig. P5.64, is held stationary by the horizontal force, Fx, and the vertical force, Fz. The velocity and pressure of the exhaust gas are 5000 ft/s and 20 psia at the nozzle exit, which has a cross section area of 60 in.2 . The exhaust mass flowrate is constant at 21 lbm/s. Determine the value of the restraining force Fx. Assume the exhaust flow is essentially horizontal.

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