Description: From Summary: "Flutter tests have been conducted on two low-aspect-ratio wing plan forms under consideration by the Boeing Airplane Company for the 110A weapons system. These configurations had three heavy nacelles near the trailing edge, and flutter tests were made both with and without the nacelles. Up to a Mach number of 3.0 the dynamic pressure required for flutter of a wing with nacelles was generally higher than that of a wing without nacelles."
Date: October 24, 1957
Creator: Levey, G. M.; Tuovila, W. J. & Rainey, A. G.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department