Tabulated pressure coefficients and aerodynamic characteristics measured in flight on the wing of the D-558-I research airplane through a Mach number range of 0.80 to 0.89 and throughout the normal-force-coefficient range at Mach numbers of 0.61, 0.7
Description: No Description Available.
Date: August 20, 1951
Creator: Keener, Earl R; Bandish, Rozalia M & NACA
Item Type: Refine your search to only Report