Hostname: page-component-586b7cd67f-tf8b9 Total loading time: 0 Render date: 2024-11-25T05:34:00.000Z Has data issue: false hasContentIssue false
  • English
  • Français

Design of Aerofoils for Prescribed Pressure Distribution in Viscous Incompressible Flows

Published online by Cambridge University Press:  07 June 2016

H.N.V. Dutt  and
A.K. Sreekanth
H.N.V. Dutt
Affiliation:
Department of Aeronautical Engineering, Indian Institute of Technology, Madras
A.K. Sreekanth
Affiliation:
Department of Aeronautical Engineering, Indian Institute of Technology, Madras
Get access

Summary

A design procedure has been developed to generate aerofoil shapes for prescribed pressure distributions in an incompressible viscous attached flow. It is based on the method of singularities, originally proposed by Chen and later modified by Kennedy and Marsden, for inviscid flows. The classical approach of adding the displacement thickness of the boundary layer and wake to the aerofoil contour is used to account for viscous effects. Several numerical examples are worked out and are compared with the inviscid flow results. Significant changes in aerofoil contours due to viscous effects are observed and these are discussed.

Type
Research Article
Information
Aeronautical Quarterly , Volume 31 , Issue 1 , February 1980 , pp. 42 - 55
Copyright
Copyright © Royal Aeronautical Society. 1980

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1 Arlinger, B., An exact method of two-dimensional Aerofoil design. SAAB TN 67, SAAB-SCANIA. October 1970 Google Scholar
2 Kennedy, J.L. and Marsden, D.J., A potential flow design method for Multicomponent aerofoil sections. Journal of Aircraft, Vol. 15, No. 1, pp 47–52, 1978 Google Scholar
3 Chen, A.W., The determination of the geometries of multiple element aerofoils optimized for maximum lift coefficient. NASA-TM-X 67591, 1971Google Scholar
4 Oellers, H.J., Die Inkompressible potential stromung in der ebenen gitterstufe. Jahrbuch 1962, WGLR, e.v., pp 349–353 Google Scholar
5 Morgan, H.L., A computer program for the analysis of multi-element airfills in two-dimensional subsonic, viscous flows. NASA SP-347, Part II, pp 713–748 (1975)Google Scholar
6 Stevens, W.A.,, Goradia, S.H. and Braden, J.A., Mathematical model for two-dimensional Multi-component aerofoils in viscous flows. NASA CR - 1843, July 1971 Google Scholar
7 Bingham, G.J. and Chen, A.W., Low speed aerodynamic characteristics of an aerofoil optimized for maximum lift coefficient. NASA TN D - 7071 (1972)Google Scholar
8 McGhee, R.J. and Beasley, W.D., Low speed aerodynamic characteristics of a 17% thick aerofoil section designed for general aviation applications. NASA TN D - 7428, 1973 Google Scholar