Quarterly of Applied Mathematics

Quarterly of Applied Mathematics

Online ISSN 1552-4485; Print ISSN 0033-569X

   
 
 

 

The design of two-dimensional aerofoils with mixed boundary conditions


Author: L. C. Woods
Journal: Quart. Appl. Math. 13 (1955), 139-146
MSC: Primary 76.1X
DOI: https://doi.org/10.1090/qam/68973
MathSciNet review: 68973
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Abstract: A method is given of designing two-dimensional symmetrical aerofoils in subsonic compressible flow when the boundary conditions are mixed. The aerofoil surface is divided into three parts such that the shape is prescribed in the first and third and the pressure distribution is specified in the second. The method has the advantage over the usual method of aerofoil design (pressure distribution given over the whole aerofoil surface) of giving the designer direct control of the nose shape and the trailing edge angle.


References [Enhancements On Off] (What's this?)

  • [1] M. J. Lighthill, A new method of two-dimensional aerodynamic design, British Aero. Res. Council R. & M. 2112 (1945)
  • [2] L. C. Woods, Aerofoil design in two-dimensional subsonic flow, British Aero. Res. Council R. & M. 2845 (1952) MR 0079463
  • [3] L. C. Woods, Compressible subsonic flow in two-dimensional channels with mixed boundary conditions, to be published shortly in the Quart. J. Mech. and Appl. Math. MR 0065340
  • [4] L. C. Woods, The application of the polygon method to the calculation of the compressible subsonic flow round two-dimensional profiles, British Aero. Res. Council Current Paper No. 115 (1952) MR 0059130
  • [5] G. Birkhoff, Hydrodynamics: A study in logic, fact and similitude, Princeton University Press, 1950 MR 0038180
  • [6] Th. von Kármán, Compressibility effect in aerodynamics, J. Aero. Sci. 8, No. 9 (1941) MR 0005848

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DOI: https://doi.org/10.1090/qam/68973
Article copyright: © Copyright 1955 American Mathematical Society

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