TECHNICAL MEMORANDUM - CORE
The left main landing gear (MLG) began a violent shimmy (yaw oscillation) when the wheelbrakes were applied after a normal landing touchdown, probably damaging ...
Influence of variable side-stay geometry on the shimmy dynamics of ...... shimmy) and rotational-dominant shimmy regions. Comparing ... Burton TD (1981) Describing function analysis of nonlinear nose gear shimmy. Influence of Variable Side-Stay Geometry on the Shimmy Dynamics ...Dur- ing this initial time integration, the landing gear touchdown on the runway is simulated. The system is integrated in time until the ... 1.1 Aircraft Type and Registration: Boeing 737-59D, G-BVKC No & TypHence. Page 51. NACA TM 1337. For C2 Kantrowitz obtained C2 = 6.2 feet, or C2 = 0.2. (c.G.s. system). Calculation of T. D. S. R. and G. Coefficient ? has ...
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