Effect of Mach number on the maximum lift and buffeting boundary determined in  flight on a north american P-51D airplane (open access)

Effect of Mach number on the maximum lift and buffeting boundary determined in flight on a north american P-51D airplane

Flight tests were conducted on a North American P-51D airplane to establish the maximum lift coefficient and the buffeting boundary line as a function of Mach number.
Date: June 12, 1947
Creator: Mayer, John P.
System: The UNT Digital Library