Tests of a 1/14-Scale Powered Model of the XB-36 Airplane in the Langley 19-Foot Pressure Tunnel I : Stalling Characteristics and Aileron Effectiveness of Several Wing and Flap Arrangements
1945-02-01
Sonstige
Keine Angabe
Englisch
WINGS - CONSOLIDATED VULTEE B-36 WIND TUNNEL TESTS (NACA - PRESSURE-19') , WING FLAPS, SPLIT - BALANCED , AIRPLANES - CONSOLIDATED VULTEE B-36 (EXPERIMENTAL) WIND TUNNEL - TESTS (NACA - , WING SPOILERS , WING FLAPS, SLOTTED - PARTIAL-SPAN , AILERONS - CONSOLIDATED VULTEE B-36 , WING FLAPS, FULL-SPAN , STALLING CHARACTERISTICS - CONSOLIDATED VULTEE B-36
Aerodynamic tests of full-scale TBF-1 Aileron installation in Langley 16-foot high-speed tunnel
Engineering Index Backfile | 1944
|Engineering Index Backfile | 1942
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