Determine the range(s) of inlet stagnation pressures for which the nozzle will be free from normal shocks.

A converging-diverging nozzle, with Ae/At 5 1.633, is

designed to operate with atmospheric pressure at the exit

plane. Determine the range(s) of inlet stagnation pressures

for which the nozzle will be free from normal shocks.

13.106 Air flows through a converging-diverging nozzle with

Ae/At 5 1.87. Upstream, T01 5 240

F and p01 5 100 psia.

The back pressure is maintained at 40 psia. Determine the

Mach number and flow speed in the nozzle exit plane.

find the cost of your paper

Calculate the maximum achievable bridge out-of-balance voltage for an applied torque T of 103 N m given the following

Four strain gauges, with specification given below, are available to measure the torque on a cylindrical shaft 4 cm in diameter connecting a motor and load. (a) Draw clearly labelled….

Find the gain and phase characteristics of the maintaining amplifier.

A solid-state capacitive humidity sensor has a capacitance given by: C = 1.7 RH + 365pF where RH is the percentage relative humidity. The sensor has an associated parallel resistance….

calculate the mean velocity of the gas at maximum flow rate

A pitot tube is used to measure the mean velocity of high pressure gas in a 0.15 m diameter pipe. At maximum flow rate the mean pitot differential pressure is….