New PDF release: Aircraft Landing Gear Design: Principles and Practices (AIAA

By Norman S. Currey

This can be the one ebook to be had at the present time that covers army and advertisement plane touchdown equipment layout. it's a complete textual content that may lead scholars and engineers from the preliminary options of touchdown apparatus layout via ultimate aspect layout. The e-book offers a necessary hyperlink in touchdown apparatus layout expertise from old practices to fashionable layout developments, and it considers the mandatory airfield interface with touchdown equipment layout. The textual content is subsidized up through calculations, requirements, references, operating examples.

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Additional info for Aircraft Landing Gear Design: Principles and Practices (AIAA Education Series)

Sample text

1~ i~JJl ,"~ i I'%'kLi_ I ltl I i I i I " LiS,',,~~~-'LL " 3:)ilillv]r"r':i ... -0°---... - Ii iill _" _. -! l~ZIZl I 1 i i i i il i IE,~[ :_1-1-1-1 i ~-! i!!! ~ Ii il . '71. ~I. Q~ o.. ->>~ I ~r ii i all. g. g. position. 07 must not exceed the tire's static load rating. g. 31 g forward (reacted by brakes). 07 factor, must not exceed the tire's dynamic rating. g. 20g forward (reacted by brakes). 07 factor, must not exceed the tire's dynamic rating. Nose wheel tire inflation pressures are based on maximum allowable dynamic loads.

O o ~. '=-~~=. =;= _ - g ~. o'z z ... 14")'-" o-- ~®~ . 1 Typical Airspeed Limits, knots Airspeed limits Air vehicle type Gear down Retract Extend Emergency extend A-7 A-10 244 200 220 200 220 200 180 200 B-52 B-57 B-66 305 200 250 220 200 250 305 200 250 305 200 250 F-4 250 250 250 250 F-5A/B F-5E F- 15 F-16 F- 100 F-105 F-106 F-I II 240 260 300 300 230 275 280 295 240 260 300 300 230 240 280 295 240 260 300 300 230 275 280 295 240 260 250 300 230 275 250 295 T-37 T-38 T-39 150 240 180 150 240 180 150 240 180 150 240 180 Source: MIL-L-87139.

7 lb. With two tires per aircraft, a weight penalty of 27 lb is thus paid to obtain the lower tire pressure. To place the tires in the deflected vertical position, note their loaded radii on the tire selection charts. 2 in. This is the distance from the ground to the axle center with the aircraft static and the tire at optimum deflection. The nose gear tire is a bit more complicated: by definition, its tire deflection will be 48% under dynamic loads appropriate for I0 ft/s/s braking. 6 tire), it is possible to determine the deflection with the static nose gear load.

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Aircraft Landing Gear Design: Principles and Practices (AIAA Education Series) by Norman S. Currey


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