Drag of straight and swept wings between parallel walls at high subsonic Mach numbers as well as at Mach numbers in transonic and supersonic ranges; object is to provide estimation of wall interferences and thus of magnitude of effective sweep angle of wings between parallel walls in transonic range.
Transonic flow past swept and unswept wings between parallel walls
Stockholm. Flygtekniska Forsoksanstalten (Aeronautical Research Inst, Sweden) -- Report
1954
34 pages
Bibliography
Report
Englisch
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