Tests of N.A.C.A. airfoils in the variable-density wind tunnel Series 24 (1932)
NASA Technical Reports Server (NTRS) · leaf 28
Ratio of Lift to Drag, L/d B3 Lj i-J M (M CD W O*^*-* "l^™ S",. 00 Center of pressuTG in ^ of Chord from Leading Edge. … <jO o Lift Coefficient (Atsolute), C^ • M s _ to CO w A3 M o o A3 00 O cn 00 Drag Coefficient (Absolute), Cjj
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
