Approximate theory of flow about slender bodies and wings originated by M.M.MUNK and R.T.JONES, reviewed; relation to source-sink methods of T. von KARMAN and others; extension to noncircular bodies for subsonic flow; interpreting Jones slender wing result as first term of expansion in powers of breadth parameter, it is shown how more accurate theory can be developed.
Slender-body theory -- Review and extension
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 20 , n 2
1953
14 pages
Bibliography
Article (Journal)
English
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