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 (Listing Multiple Pages).
This report has 171 pages. Select a thumbnail to view a larger version. Result listing will show up to 100 pages per screen. Displaying: 1 of 2.