Aerothermodynamics (SESA3029)
University of Southampton (UOS)
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Method of Characteristics Methodology
- Other • 3 pages • 2023
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This report provides a concise explanation of the MoC methodology.
A spreadsheet for a computed Mach angle and Prandtl-Meyer function for γ=1.25 and Mach number Mdes 2.4 is shown. The spreadsheet is verified to give the correct values.
A plot of the design of the shape of the nozzle is shown and a short discussion of results is included and a comparison with quasi 1D theory is given (i.e. A/A* for γ and Mdes) and a discussion of limitations of the procedure is provided.
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Method of Characteristics Methodology
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This report provides a concise explanation of the MoC methodology. A spreadsheet for a computed Mach angle and Prandtl-Meyer function for γ=1.25 and Mach number Mdes 2.4 is shown. The spreadsheet is verified to give the correct values. A plot of the design of the shape of the nozzle is shown and a short discussion of results is included and a comparison with quasi 1D theory is given (i.e. A/A* for γ and Mdes) and a discussion of limitations of the procedure is provided.
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