blob: 150e6c99da1aa65bd12f6f32ebc59622807e2918 (
plain)
1
2
3
4
5
6
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,
|
