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Relation Between the Stability Characteristics and the Controllability of German Airplanes (1930)

NASA Technical Reports Server (NTRS) · leaf 28

An illustration from Relation Between the Stability Characteristics and the Controllability of German Airplanes, 1930, leaf 28
Fig.9 Elevator with balancing sur- face on a Junkers F.13 f.e. Fig.10 Internally balanced rudder and elevator on the Albatros L.76 airplane. Fig.11 Auxiliary balance on eleva- tor of Dornier Merkur air- plane. The rudder has a balancing surface

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