Aerospace Engineering > GATE 2014 > Ramjet Engines
A cruise missile with an ideal ramjet engine is flying at Mach 4.0 at an altitude where the ambient temperature is 100K. Considerratio of specific heatsy =1.4 and specific gas constant R=287J/kgK If the stagnation temperature in the combustion chamber is equal to 2310K, the speed of the exhaust gases (in m/s) is
Correct : 1880 to 1881
Similar Questions
Which one of the following shows the CORRECT variation of stagnation temperature along the axis of an ideal ram jet engine?
Which one of the following shows the CORRECT variation of stagnation temperature along the axis of an ideal ram jet engine?
Which one of the following shows the CORRECT variation of stagnation temperature along the axis of an ideal ram jet engine?
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