*Eric Reissner*

*naca-tn-2363*

*May 1951*

An account is given of explicit solutions in terms of Mathieu function functions of the problem of two-dimensional subsonic compressible flow past oscillating airfoils. The results are applied to the calculation of three-dimensional corrections for the two-dimensional theory and the effect of the incorporation of the three-dimensional theory effect on the Mathieu function solution of the two-dimensional problem is shown.

*An Adobe Acrobat (PDF) file of the entire report:*

http://naca.central.cranfield.ac.uk/reports/1951/naca-tn-2363.pdf