The Reduction in Drag of a Forward-sloping Windshield (1933)
NASA Technical Reports Server (NTRS) · leaf 6
Figure 1.-Sketch of flow about original \ri.ndshieli. … # - O / // / windshield. Ordinal form o i -4-> •H —.4. .4 ! ,p / 1 ^ Wijji^ and fuselage with wi&lsliisl kal fo: .2 r Mr I o° 1 0 X2 .04 .06 .08 Drag coefficient, 0j Figure 4.-Polar cirves showing effects of windslaield
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
