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Evaluation of Two-Dimensional Subsonic Oscillatory Airforce Coefficients and Loading Distributions

Published online by Cambridge University Press:  07 June 2016

Deborah J. Salmond
Deborah J. Salmond*
Affiliation:
Royal Aircraft Establishment, Farnborough, Hampshire
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Summary

A method is described for calculating numerically the aerodynamic stiffness and damping coefficients and loading distributions for a two-dimensional thin aerofoil oscillating harmonically in subsonic flow, from the Possio Integral Equation by approximating the loading by a finite series of basis functions. Sample loading distributions obtained by using the method are presented for a Mach number of 0.9 and a frequency parameter of 0.4.

Type
Research Article
Information
Aeronautical Quarterly , Volume 32 , Issue 3 , August 1981 , pp. 199 - 211
Copyright
Copyright © Royal Aeronautical Society. 1981

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References

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