Lift and Drag Tests of Three Airfoil Models with Fowler Flaps Submitted by Consolidated Aircraft Corporation
1941-12-01
Miscellaneous
No indication
English
AIRFOILS, GLOVE , AIRFOILS - NACA 65,2-221 - 66,2X-416 - CHAR , LOW-DRAG (WING FLAPS, FOWLER) , WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE (7 1/2' X 3') , WING FLAPS - FOWLER , WING FLAPS - DEFLECTION , AIRFOILS - DAVIS - CHARACTERISTICS - LAMINAR-FLOW (WING FLAPS, FOWLER ) , WINGS CONSOLIDATED B-32 WIND TUNNEL TESTS (NACA - 2-DIM PRESSURE)