Hostname: page-component-cd9895bd7-q99xh Total loading time: 0 Render date: 2024-12-22T15:49:00.474Z Has data issue: false hasContentIssue false
  • English
  • Français

A Thin Aerofoil of Small Camber in a Non-Uniform Flow

Published online by Cambridge University Press:  04 July 2016

L. N. Nigam
L. N. Nigam*
Affiliation:
Indian Institute of Technology, Bombay
Get access Rights & Permissions [Opens in a new window]

Extract

The direct problem of aerodynamics (profile of the aerofoil is given—calculate the aerodynamic characteristics) has been studied for thin aerofoils with small camber. Given the undisturbed stream function

V, ω, α being the constant velocity, vorticity and angle of incidence respectively, the pressure distribution, lift coefficient and pitching moment have been calculated for a general profile.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 71 , Issue 675 , March 1967 , pp. 214 - 216
Copyright
Copyright © Royal Aeronautical Society 1967

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.Tsien, H. S.QAM, Vol 1, p 130, 1943.Google Scholar
2.Munk, M. M.Rep Nat Adv Comm Aero, Wash, p 142, 1922.Google Scholar
3.Glauert, H.The Elements of Aerofoil and Air Screw Theory. Camb Univ Press, 1947.Google Scholar
4.Birnbaum, W.ZAMM, Vol 3, p 290, 1923.Google Scholar
5.Lighthill, M. J.Aeronautical Quarterly, Vol 3, p 193, 1951.CrossRefGoogle Scholar
6.Thwaites, B.Incompressible Aerodynamics, p 123. Clarendon Press, Oxford, 1960.Google Scholar
7.Milne-Thomson, L. M.Theoretical Aerodynamics, pp 140–141. Macmillan & Co, London, 1952.Google Scholar