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Generalisation of Watson’s Formulae and Applications to Aerofoil Theory
Published online by Cambridge University Press: 07 June 2016
Summary
This paper presents a contribution to Watson’s formulae and gives analogous formulae for the higher derivatives of the functions ψm and ϵm of classical aerofoil theory. In Appendix A these formulae are related to Thwaites’s method of solving Theodorsen’s non-linear integral equation. The resultant equations are also given in matrix form, which enables the calculations to be mechanised by using automatic computers.
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- Research Article
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- Copyright © Royal Aeronautical Society. 1973