Non-stationary motion of purely supersonic wings
A general theory is presented for the calculation of the total forces acting on purely supersonic wings. The method applies to wings having an arbitrary downwash distribution (stationary or non-stationary) and is valid whenever all of the wing edges are supersonic. The general three-dimensional non-...
Internet
https://thesis.library.caltech.edu/622/1/Froehlich_je_1950.pdfFroehlich, J. E. (1950) Non-stationary motion of purely supersonic wings. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/FCGZ-7P23. https://resolver.caltech.edu/CaltechETD:etd-02122009-155907 <https://resolver.caltech.edu/CaltechETD:etd-02122009-155907>