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Exact(5)
Furthermore, the value of optimum pressure ratio rf for maximum specific thrust increases with TIT.
Variations of maximum specific thrust with freestream Mach numbers and material temperature limit are analyzed respectively.
Moreover, the maximum specific thrust can also be achieved with a fuel equivalence ratio near this range.
The aim of this work is to provide an upper estimate of the theoretical maximum specific thrust of the hydrocarbon fueled scramjet.
Different with the ideal Brayton cycles assuming isentropic compression without upper limit of gas temperature, both the maximum specific thrust and the maximum fuel impulse of a scramjet present non-monotonic trends against the fuel equivalence ratio in this study.
Similar(54)
The optimum inlet pressure ratio and fuel equivalence ratio at which the value of the specific thrust attains a maximum are presented.
The results show that the specific thrust initially grows asymptotically with fuel equivalence ratio, then reaches a maximum, and finally reduces rapidly for a given flight Mach number.
maximum specific growth rate.
Maximum specific growth rate (h−1).
The underlying motivation is to reduce specific thrust and improve propulsive efficiency.
These variables affect the specific thrust and specific fuel consumption (SFC), which represent the main performance parameters.
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