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Experimental investigation of the cornering of a C40 x 14-21 cantilever aircraft tire (1973)

Dreher, R. C. ; Tanner, J. A.

In: CASI

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Publication Date: 2019-06-27

Description: An experimental investigation was conducted at the Langley aircraft landing loads and traction facility to define the cornering characteristics of a size C40 x14-21 aircraft tire of cantilever design. These characteristics, which include the cornering-force and drag-force friction coefficients and self-alining torque, were obtained for the tire operating on dry, damp, and flooded runway surfaces over a range of yaw angles from 0 deg to 20 deg and at ground speeds of 5 to 100 knots, both with and without braking. The results of this investigation show that the cornering-force and drag-force friction coefficients and self-alining torque were influenced by the yaw angle, ground speed, brake torque, surface wetness, and the locked-wheel condition.

Keywords: AIRCRAFT

Type: NASA-TN-D-7203 , L-8766

Format: application/pdf

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