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Diffstat (limited to '3685/CH21/EX21.6/Ex21_6.txt')
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diff --git a/3685/CH21/EX21.6/Ex21_6.txt b/3685/CH21/EX21.6/Ex21_6.txt new file mode 100644 index 000000000..150e6c99d --- /dev/null +++ b/3685/CH21/EX21.6/Ex21_6.txt @@ -0,0 +1,7 @@ +
+ Example 21.6
+
+ Air-fuel ratio = 60.922165,
+ Thrust power of the propeller = 4144.338339 kJ/s ,
+ Thrust by the propeller = 26.523765 kN,
+ Mass flow rate of air flowing through the compressor = 27.435823 kg/s,
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