Conclusion
The method of graphical computation based on the use of characteristics is easier to handle than the arithmetical computation for the study of unsteady flow problems. The possibility of reducing the equations for the characteristics into simple non-dimensional form gives the construction an accuracy comparable with the numerical computation. Regarding the results obtained by this method, it is necessary to verify by actual measurements on pipe flows and engine trials the validity of the simple assumptions made in the graphical computation. The success of the method indicates that it may be possible to use this procedure for the case of the parallel supersonic jet also. In fact the method of characteristics has been successfully employed in the design of a parallel flow jet in some recent work by R. Saurer5 and K. Foetsch.6
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References
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(Communicated by Dr. B. R. Seth)
Numbers marked within brackets refer to the references cited at the end of the paper.
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Murthy, S.N.B. On the characteristic method for unsteady compressible flow. Proc. Indian Acad. Sci. 37, 664–680 (1953). https://doi.org/10.1007/BF03052695
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DOI: https://doi.org/10.1007/BF03052695