Question

please draw T-S and P-V diagrams relevant to the DGEN380 engine cycle identifying the actual station numbering ( not to scale )

ral Information the following engine section numbering: Retale 4145 S 25 Fig3.1: Engine Section Numbering Location Station Number Front Fan Face 21 Gooseneck Inlet Compressor Inlet Diffuser Exit Combustion Chamber Exit HP Turbine Inlet HP Turbine Exit LP Turbine Inlet LP Turbine Exit Core Stream Exit Fan Stream Exit 25 41 45 18 Table3.I: Section Numbering Identification Draw the T-S and P-V Diagrams relevant to the DGEN380 engine cycle identifying the actual station numberingて may not be to scale).

Answer 1

(18) Bypass Nozzle I T Core stream exit 2ら Front Fon- face Compressor Diffuser inlet exit ㄒ PT 3 41 41 LPT 5 COMREsSOR DIFFUSER N02ZLE 5 25 251 8 2. P v Diagram 下S Diagram