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List of Figures Figure 1: Preliminary engine design process [10] ................................................................................. 16 Figure 2: Different cycle efficiencies over velocity ratio in the mixer................................................... 19 Figure 3: 𝜂𝑡h over OPR for different types of cycles [11].................................................................... 20 Figure 4: Velocity triangles for a typical compressor stage [19] ........................................................... 22 Figure 5: Different types of flow paths.................................................................................................. 23 Figure 6: Typical burner [22] ................................................................................................................. 25 Figure 7: Theoretical thrust gain due to mixing [11]............................................................................. 26 Figure 8: Different types of disc designs [28] ........................................................................................ 28 Figure 9: Section view baseline engine ................................................................................................. 29 Figure 10: Engine layout with flow stations .......................................................................................... 30 Figure 11: Optimum OPR at different TIT: s. ......................................................................................... 31 Figure 12: Efficiencies over OPR............................................................................................................ 32 Figure 13: The MJ – Haran S14 section view ......................................................................................... 33 Figure 14: The MJ – Haran S14 section view with supersonic inlet ...................................................... 33 Figure 15: Supersonic inlet with flow stations ...................................................................................... 34 Figure 16: Ducts..................................................................................................................................... 35 Figure 17: Stage load over flow coefficient for the FAN and HPC......................................................... 35 Figure 18: Fan component .................................................................................................................... 35 Figure 19: Velocity triangles for the fan at mean blade ........................................................................ 36 Figure 20: HPC component.................................................................................................................... 37 Figure 21: Velocity triangles for the HPC at mean blade ...................................................................... 38 Figure 22: Combustor component ........................................................................................................ 38 Figure 23: Stage load over flow coefficient for the HPT and LPT .......................................................... 39 Figure 24: HPT component.................................................................................................................... 39 Figure 25: Velocity triangles for the HPT at mean blade....................................................................... 40 Figure 26: LPT component..................................................................................................................... 41 Figure 27: Velocity triangles for the LPT at mean blade ....................................................................... 42 Figure 28: Mixer component ................................................................................................................. 42 Figure 29: Nozzle component................................................................................................................ 43 Figure 30: Rate of change in area over distance and area over distance for the nozzle ...................... 43 Figure 31: First stage HPC disc output file from T-AXI DISC .................................................................. 44 Figure 32: Typical mission for the engine.............................................................................................. 45 viiiPDF Image | Conceptual Design of a Supersonic Jet Engine
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