Wind-tunnel research comparing lateral control devices, particularly at high angles of attack V : spoilers and ailerons on rectangular wings (1933)
NASA Technical Reports Server (NTRS) · leaf 5
724 REPORT NATIONAL ADVISORY COMMITTEE FOB AERONAUTICS Aileron angle, SA up only Aileron angle, SA up only Fiqtob 9.—Boiling and yawing moment coefficients due to spoiler B op 90° and Fioube 10.—Boning and yawing moment coefficients doe to spoiler 0 up 00° and. standard ailerons short, wide ailerons … a.,per cent b/2 Angle of attack, ol Figuee 11.—Effect ol span location of spoiler on rolling and yawing moment coeffi- Fiqcbe 12.—Effect of spoiler sire on rolling and yawing momont coeffi- cients due to spoiler D and short, wide ailerons. 33=90°; Sx-(fp up only cients due to spoiler D and short,…
NASA Technical Reports Server (NTRS)
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