In the static test of a jet engine and exhaust nozzle assembly, air is sucked into the
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In the static test of a jet engine and exhaust nozzle assembly, air is sucked into the engine at the rate of 30 kg /s and fuel is burned at the rate of 1.6 kg/s. The flow area, static pressure, and axial-flow velocity for the three sections shown are as follows:
Sec. A Sec. B Sec. C
Flow area, m2 0.15 0.16 0.06
Static pressure, kPa −14 140 14
Axial-flow velocity, m/s 120 315 600
Determine the tension T in the diagonal member of the supporting test stand and calculate the force F exerted on the nozzle flange at B by the bolts and gasket to hold the nozzle to the engine housing.
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Related Book For
Engineering Mechanics Dynamics
ISBN: 9781118885840
8th Edition
Authors: James L. Meriam, L. G. Kraige, J. N. Bolton
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