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

February 14, 2018 | Aerospace | By admin | 0 Comments

By Norman S. Currey

This can be the one booklet on hand this day that covers army and advertisement plane touchdown equipment layout. it's a complete textual content that might lead scholars and engineers from the preliminary recommendations of touchdown equipment layout via ultimate aspect layout. The e-book offers an important hyperlink in touchdown equipment layout expertise from old practices to trendy layout developments, and it considers the mandatory airfield interface with touchdown apparatus layout. The textual content is subsidized up via calculations, standards, references, operating examples.

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

Example text

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. In addition to the above, the BCAR includes tests for static force, reduced speed stopping, overload, and certified emergency brake energy.

TAN. ,. Y Fig. 7 Turnover angle calculation. relatively narrow-track gears mounted on the fuselage. De Havilland Canada aircraft such as the DHC-5, Dash-7, and Dash-8 have nacellemounted gears with a consequent reduction in the turnover angle. 8 shows the DHC-5 nacelle-mounted arrangement. Another approach is to use a bicycle-type gear, as on the B-47, with outrigger wheels between the siamese engine nacelles to restrict turnover. This is illustrated in Fig. 9. Figure 3. I0 depicts a method that was used by the author some years ago on a design that did not proceed beyond the study stage.

Along these lines. g. position is generally of little importance in the determination of aircraft configurations, its position will probably not have been calculated at this stage and a "guesstimate" must be made. , so if the aircraft is, for instance, a high-wing cargo aircraft, an approximate calculation will be made assuming full wing fuel and no cargo. A low-wing passenger aircraft would be critical with no wing fuel and a full load of passengers. In step 4, from observations of wing spar locations and other structure, the main gear is placed in a position that appears to be the most conducive to the efficient transmission of loads.

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


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