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nhanshikendoLv1
21 Oct 2023
Triple-spool unmixed turbofan engine (Trent 700) is shown in Fig. 2. Bleed air having a percentage of 8 % is taken from HP compressor to cool HP and IP turbines as shown in Fig.3. Engine has the following data in Table 1 below: For takeoff operation where Mach number M=0.2 at sea level, calculate: 1. The total temperature at the outlet of the fan and intermediate- and high-pressure compressors 2. The total temperature at the outlet of the high-, intermediate-, and low-pressure Turbines 3. The pressure and temperature at the outlet of cold and hot nozzles 4. Specific thrust, thrust specific fuel consumption, and propulsive, thermal, and overall efficiencies
Triple-spool unmixed turbofan engine (Trent 700) is shown in Fig. 2. Bleed air having a percentage of 8 % is taken from HP compressor to cool HP and IP turbines as shown in Fig.3. Engine has the following data in Table 1 below: For takeoff operation where Mach number M=0.2 at sea level, calculate: 1. The total temperature at the outlet of the fan and intermediate- and high-pressure compressors 2. The total temperature at the outlet of the high-, intermediate-, and low-pressure Turbines 3. The pressure and temperature at the outlet of cold and hot nozzles 4. Specific thrust, thrust specific fuel consumption, and propulsive, thermal, and overall efficiencies
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