Full Scale Span Load Distribution on a Tapered Wing with Split Flaps of Various Spans (1937)
NASA Technical Reports Server (NTRS) · leaf 15
r ! | i i i f Airfoil: Tapered U.S.A. 45 Size: 7.38 (mean chord) by 45.75 feet -4 flap: 20 % chord, y7.6 ;.fe span / … Distance from leading edge of section chord in percentage of sectim chord "ft Figure 5.- Typical section pressure diagrams. CJ1
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
