Wind-tunnel research comparing lateral control devices, particularly at high angles of attack I : ordinary ailerons on rectangular wings (1933)
NASA Technical Reports Server (NTRS) · leaf 2
AR WINGS the balances, and auxiliary apparatus are described in the right and left ailerons throughout the range of detail in reference 2. displacement with the two differential arrangements. For ordinary force tests the model is mounted on a These are illustrated in Figure 2, which also shows the… … cause of the different wing-load distribution, prelimi- D, Up-only nary tests were made which showed good agreement Fiqube 2.—Aileron linkage systems—assumed TTKnrtniniii defleotionj within the accuracy of the investigation. The final TABLE I tests were made with the ailerons deflected equal and…
NASA Technical Reports Server (NTRS)
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