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On diffuser efficiency in compressible flow

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An Erratum to this article was published on 01 November 1945

Summary

An expression for diffuser efficiency in compressible flow has been developed. Experimental procedures for the determination of the efficiency are outlined and the steps for calculating it from the experimental data are indicated.

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References

  1. Parkinson “Modern Diffuser Design,”Aircraft Engineering, 1938,10, 267.

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  2. Ackeret “High Speed Wind Tunnels,”N. A. C. A. Tech. Memo., 1936, No. 808.

  3. CrocoAtti dell’ Associazione Italiana di Aerotecnica, 1939–40,19.

  4. GlauertAerofoil and Airscrew Theory, Cambridge University Press, 1926.

  5. BatemanBulletin of the National Research Council, Washington, D.C., 1931, No. 84, 469.

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Authors
  1. P. Nilakantan
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Additional information

(Communicated by Sir C V. Raman, Kt.,f.r.s., n.l.)

An erratum to this article is available at http://dx.doi.org/10.1007/BF03173960.

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Nilakantan, P. On diffuser efficiency in compressible flow. Proc. Indian Acad. Sci. (Math. Sci.) 22, 67 (1945). https://doi.org/10.1007/BF03170913

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  • DOI: https://doi.org/10.1007/BF03170913

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