Theoretical stability and control characteristics of wings with various amounts of taper and twist (1938)
NASA Technical Reports Server (NTRS) · leaf 3
THEORETICAL STABILITY AND CONTROL CHARACTERISTICS OF WINGS Relative distance from wing center (a) X=L00. Cb] W1JS0. Co) X-0.25. Ficcbi 2.—Load distribution dne to nnlt angles of attaok extending Inward from the tip.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
