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Dynamic and Flight Tests on Rubber-Cord and Oleo-Rubber-Disk Landing Gears for an F6C-4 Airplane (1932)

NASA Technical Reports Server (NTRS) · leaf 14

An illustration from Dynamic and Flight Tests on Rubber-Cord and Oleo-Rubber-Disk Landing Gears for an F6C-4 Airplane, 1932, leaf 14
13 FLIGHT TESTS ON LANDING GEARS FOR AN F6C-4 AIRPLANE 28 \t)28 ■6 l24 ! u r I 12 0 0 8- % .1: 36 4 8 12 16 20 24 28 32 4 8 12 16 20 24 28 32 36 Total vertical drop of landing gear, inches Total verfical drop of londino oeor, inches Figure 21.—Relation between total drop and free drop for the oleo… … Time, sec. Figure 23.—Pressure histories for oleo cylinders; l^i-inch free drop 800.^ 2320 lb. sfoiic load on tires 600\^ (1735 lb. plot form load). 400 ^ 200^ .20 .24 0 .04 Time, sec. [^'iGUKE 21.—Pressure histories for oico cylinders

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