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A ramjet engine is analyzed using the air standard method. Given specific operating conditions determine the...

A ramjet engine is analyzed using the air standard method. Given specific operating conditions determine the temperature, pressure, and enthalpy at each state, the exit velocity, and the rate of heat addition (kJ/kg).

--Given Values--

T1 (K) = 236

P1 (kPa) = 54

V1 (m/s) = 632

rc = 2.03

a) Determine the specific enthalpy (kJ/kg) at state 1.

b) Determine the relative pressure at state 1.

c) Determine the specific enthalpy (kJ/kg) at state 2.

d) Determine the temperature (K) at state 2.

e) Determine the relative pressure at state 2.

f) Determine the pressure (kPa) at state 2.

g) Determine the temperature (K) at state 3.

h) Determine the specific enthalpy (kJ/kg) at state 3.

i) Determine the relative pressure at state 3.

j) Determine the relative pressure at state 4.

k) Determine the specific enthalpy (kJ/kg) at state 4.

l) Determine the velocity (m/s) at the exit of the turbojet engine.

m) Determine the rate of heat addition (kJ/kg).

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Answer #1

Given sine = 236K P = Se kPa = T2 9.03 Pi Tamperature ar state2. astete 2. A ramjet engine is analysed using the air standard

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