Browsing Aeronautical Research Council by Author "Sylvia W. Skan"

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Aerodynamic Forces on Biconvex Aerofoils Oscillating in a Supersonic Airstream + Effect of Thickness on the Aerodynamic Forces on Biconvex Aerofoils Oscillating in a Supersonic Airstream, and Calculation of Forces for Aerofoil with Flap

W. P. Jones; Sylvia W. Skan (1951)

A method for the calculation of the aerodynamic forces on an oscillating aerofoil which allows for the effect of thickness is developed. The steady flow regime for zero or mean incidence is first determhaed for isentropic, ...
Possio's subsonic derivative theory and its application to flexural-torsional wing flutter parts 1 and 2

R. A. Frazer; Sylvia W. Skan (1942)

Part I. Possio's Derivative Theory for an Infinite Aerofoil Moving at Subsonic Speeds. The derivative theory due to C. Possio for an infinite aerofoil moving at subsonic speeds is reviewed, and certain modifications are ...

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