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diff --git a/3685/CH13/EX13.10/Ex13_10.txt b/3685/CH13/EX13.10/Ex13_10.txt new file mode 100644 index 000000000..64d78442e --- /dev/null +++ b/3685/CH13/EX13.10/Ex13_10.txt @@ -0,0 +1,7 @@ +
+ Example 13.10
+
+ The temperature of the gases at the turbine exit is 1114.474397 K,
+ The pressure of the gases at the turbine exit is 311.998817 kN/m^2,
+ The velocity of gases at the nozzle exit is 1020.347840 m/sec,
+ The propulsive efficiency of the cycle is 25.699731 percent
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