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| author | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
|---|---|---|
| committer | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
| commit | 7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 (patch) | |
| tree | dbb9e3ddb5fc829e7c5c7e6be99b2c4ba356132c /3685/CH21/EX21.6/Ex21_6.txt | |
| parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
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initial commit / add all books
Diffstat (limited to '3685/CH21/EX21.6/Ex21_6.txt')
| -rw-r--r-- | 3685/CH21/EX21.6/Ex21_6.txt | 7 |
1 files changed, 7 insertions, 0 deletions
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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