Wind-tunnel research comparing lateral control devices, particularly at high angles of attack III : ordinary ailerons rigged up 10 degrees when neutral (1933)
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of the results in this re- ance with the standard procedure, and at the dynamic port is the same as that in Part I. (Reference 1.) It pressure and Reynolds Number employed throughout is considered satisfactory at all angles of attack except the entire series of investigations on lateral control. in… … This coefficient may be used as a measure of the D, Up-only degree of lateral stability or instability of a wing under Tig dbe 4. Aileron linkage systems. Assnmed maximum deflection with the neu- tral 10° up various rolling conditions. In the present case, it is used to indicate the characteristics…
NASA Technical Reports Server (NTRS)
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