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Integral equations for subsonic gas flow in turbines

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Conclusions

Integral equations provide an, exact formulation for the flow in a turbine lattice; solution of the integral equation by successive approximation gives the potential and flow speed in analytical form. If (3.16) and (4.7) are met, the process also converges to the exact value. This algorithm is comparatively readily, implemented with a medium-power computer.

The result from the integral equations goes with standard results [3, 4, 7] to show that the technique is of some value in research on subsonic flows.

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Literature Cited

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Authors
  1. G. I. Chmyr'
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Additional information

Zaporozhe Engineering Institute. Translated from Prikladnaya Mekhanika, Vol. 14, No. 9, pp. 110–117, September, 1978.

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Chmyr', G.I. Integral equations for subsonic gas flow in turbines. Soviet Applied Mechanics 14, 991–997 (1978). https://doi.org/10.1007/BF00885755

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  • DOI: https://doi.org/10.1007/BF00885755

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