Norman S. Currey's Aircraft Landing Gear Design: Principles and Practices (AIAA PDF

By Norman S. Currey

This can be the one publication to be had this present day that covers army and advertisement plane touchdown apparatus layout. it's a finished textual content that may lead scholars and engineers from the preliminary options of touchdown apparatus layout via ultimate element layout. The booklet presents an essential hyperlink in touchdown equipment layout expertise from old practices to fashionable layout traits, and it considers the mandatory airfield interface with touchdown equipment layout. The textual content is sponsored up by way of calculations, necessities, references, operating examples.

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Extra resources for Aircraft Landing Gear Design: Principles and Practices (AIAA Education Series)

Example text

The brake may be cold at the beginning of each run and may be cooled between runs except that one run is used to obtain the natural cooling/time curve. Measure the stopping time for each fUll. B C A R Method 2. At least 5 stops should be made as shown in method 1, plus 95 similar stops which may be made at reduced speed to allow maximum brake usage in stopping the aircraft from the greater of the following: 1) the recommended brake application speed associated with a normal landing at the normal touchdown speed or 2) the stalling speed in the landing configuration.

These changes can include rcfairing the aft fuselage, moving or shortening belly antennas, moving the engines inboard or upward, restricting control surface deflection, and lengthening the landing gear or moving it outboard. In addition to drawings, a pitch/roll limitation diagram is often prepared, an example of which is shown in Fig. 11. ,4 k B-727 \ " . ~4 • Flap, aileron, k ~ nacelle \\\~contact Fig. 11 Pitch and roll limitation diagram. ~ 2 m 0 0 m i 2 4 Aircraft t. / I1. :. , m z..... J ~F--.

With this factor, the loads are as follows: Main gear tire load = 13,373 Ib Nose gear tire load = 3,938 Ib Nose gear braking load = 7,188 Ib The rated loads of the selected tires should be as close as possible to the above values if the minimum weight is to be realized. 2 are appropriate to this example. It is clear that several tires are capable of meeting the required load conditions. The selection, then, must be based upon factors other than load. /" Fig. 4 Final step of concept. fighter, minimum weight and size will be particularly important, irrespective of tire pressure.

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

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