Noncircular fuselages in supersonic flow
The applicability of linearized theory to the aerodynamic study of slender, three-dimensional bodies in supersonic flow is considered in detail, and figures are presented which show the limitations of body shape and mach number to be observed if quantitatively reliable results are to be achieved. T...
Internet
https://thesis.library.caltech.edu/485/1/Peterson_nc_1949.pdfPeterson, Norman Charles (1949) Noncircular fuselages in supersonic flow. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/JCZX-0749. https://resolver.caltech.edu/CaltechETD:etd-02032009-125355 <https://resolver.caltech.edu/CaltechETD:etd-02032009-125355>