Skip to main content
Log in

Note on an airfoil in a slightly non-uniform stream

  • Published:
Applied Scientific Research Aims and scope Submit manuscript

Summary

An investigation is presented of the modifications that must be made to two-dimensional calculations of the flow past an airfoil when the flow takes place in a symmetric channel with slightly non-parallel walls.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. Glauert, H., The Elements of Airfoil and Airscrew Theory, Macmillan, 1944.

  2. Dwight, H. B., Tables of Integrals, No. 815.1, Macmillan, 1961.

  3. Tricomi, N., Singular Integral Equations, p. 180, Interscience, 1957.

  4. Van Dyke, M. D., Second Order Subsonic Airfoil Theory Including Edge Effects, NACA Report 1274, 1954.

  5. Kubota, S., Bull. Jap. Soc. Mech. Eng., 5, 19 (1962), p. 450.

    Google Scholar 

  6. Pollard, D. and J. H. Horlock, A Theoretical Investigation of the Effect of Change in Axial Velocity on the Potential Flow Through a Cascade of Aerofoils, Aero. Res. Council C. P. 619, 1963 (Great Britain).

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Acosta, A.J., Mani, R. Note on an airfoil in a slightly non-uniform stream. Appl. Sci. Res. 18, 21–27 (1968). https://doi.org/10.1007/BF00382331

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF00382331

Keywords

Navigation