Investigation of boundary-layer Reynolds number for transition on an NACA 65 sub (215) sup-114 airfoil in the Langley two-dimensional low-turbulence pressure tunnel
Description: No Description Available.
Date: October 1, 1948
Creator: Braslow, A. L. & Visconti, F.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department