Analysis of Wind-Tunnel Tests to a Mach Number of 0.90 of a Four-Engine Propeller-Driven Airplane Configuration Having a Wing With 40 Degrees of Sweepback and an Aspect Ratio of 10 Page: 91 of 171. Large.

This is a large version of a page associated with this report. We provide several sizes for each page for review, download, and linking on the web.

In order to give you an accurate assessment of its downloadable size, the image below will not resize in your browser window. For larger resolution views, magnify the image with this tool and print using your browser, or contact us about copies and reproductions.