Potential flow about arbitrary biplane wing sections (1937)
NASA Technical Reports Server (NTRS) · leaf 26
73 POTENTIAL FLOW ABOUT ARBITRARY BIPLANE WING SECTIONS (a) Pressure distribution for the upper wing section of the biplane combination In figure 10. -3.0 r … (c) Pressure distribution for the monoplane airfoil section (N. A. O. A. 4112). Fiqubb 12.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
