A Flight Investigation of Laminar and Turbulent Boundary Layers Passing Through Shock Waves at Full-scale Reynolds Numbers (1953)
NASA Technical Reports Server (NTRS) · leaf 14
NACA TN 3056 l-1+7817 Figure 1.- Airplane with airfoils installed on left and right wings (prior to covering test-airfoil surfaces with aluminum sheets).
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
