Aerodynamic performance of several techniques for spike-position control of a blunt-lip nose inlet having internal contraction; Mach numbers of 0.63 and 1.5 to 2.0
Description: No Description Available.
Date: September 17, 1957
Creator: Anderson, Arthur A & Weinstein, Maynard I
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department