Tests on a model of the D.F.W. airplane T-29 of the "Deutsche Flugzeug derke" (German airplane works) (1924)
NASA Technical Reports Server (NTRS) · leaf 20
incidence relative to center line Maximum crank shaft, Mean gap Surface Chord Span t — 2 in in mm m i ram cm mm. lib 2, 5° 10' jUpper wing |775 119.66 ^.06 30.511103 772 3.9s |Rib 12 20' '101 h,05,g7 J Jlib 7, 6° 20' 755 !29.7^103 ^-06 G&3 Tjower wing (+9.30)! (+60)
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
