Determination of the characteristics of tapered wings (1937)
NASA Technical Reports Server (NTRS) · leaf 16
DETERMINATION OF THE CHARACTERISTICS OF TAPERED WINGS 1.6 1.4 o Airfoil: 00-15-3.45 R.N, (effective) 8J30,000 Dote: 3-28-34 Test: V.O.T 1178 t.2 1.4 .2 .4 .6 .6 1.0 '.2 8 12 f6 20 24 -16 -12 -6 -4 Lift coeffiriont CL Angle of attach, cf (degrees) referred to root chord Fioxjbx 19.—Tapered N. A. C.… … FlOUKB 20,-Tapered N. A. C. A. 00-15-3.45 (4:1) airfoil.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
