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Evaluation of Two-Dimensional Subsonic Oscillatory Airforce Coefficients and Loading Distributions
Published online by Cambridge University Press: 07 June 2016
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.
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- Copyright © Royal Aeronautical Society. 1981
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