A theoretical investigation of the effect of upwash and camber on drag due to lift for rectangular wings at supersonic speeds
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in .pdf document. A theoretical investigation was conducted, using linearized theory, to determine the combined effects of upwash and camber on drag due to lift for rectangular wings at supersonic spee...
Internet
https://thesis.library.caltech.edu/259/1/Seidman_o_1955.pdfSeidman, Oscar (1955) A theoretical investigation of the effect of upwash and camber on drag due to lift for rectangular wings at supersonic speeds. Engineer's thesis, California Institute of Technology. doi:10.7907/AMQ1-JJ66. https://resolver.caltech.edu/CaltechETD:etd-01212004-103434 <https://resolver.caltech.edu/CaltechETD:etd-01212004-103434>