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16-foot wind tunnel advance research results AERONAUTICS WARTIME REPORT ailerons and spoilers ailerons droop Air Materiel Command Ames Aeronautical Laboratory angle of attack Army Air Forces authorized group requiring auxiliary flaps coefficient for balance COMMITTEE FOR AERONAUTICS contour changes coolant critical Mach critical speed curves decrease divided duct diving characteristics drag coefficient elevator empennage entrance expedite general distribution figures 17 FLAP ANGLE Flap position flaps full four-engine transport airplane full stick deflection function of lateral fuselage Ilach inboard flaps inboard nacelles lateral control system lateral stick position lateral-control lift coefficient lip extension llach Mach number maximum rolling velocity miles per hour minimum speed NACA WARTIME REPORTS NATIONAL ADVISORY COMMITTEE nically edited oil-radiator duct original duct papers originally issued pilot pitching moments pitching-moment coefficient rnph Root chord rumble shown in figure shows sideslip sq ft square feet tail tests trunnion tunnel-wall effects values of pb/2V viously held