Download Aircraft Landing Gear Design: Principles and Practices (AIAA by Norman S. Currey PDF

By Norman S. Currey

This is often the single publication on hand this day that covers army and advertisement plane touchdown equipment layout. it's a finished textual content that might lead scholars and engineers from the preliminary thoughts of touchdown equipment layout via ultimate element layout. The booklet offers a necessary hyperlink in touchdown apparatus layout know-how from historic practices to fashionable layout tendencies, and it considers the mandatory airfield interface with touchdown equipment layout. The textual content is sponsored up by means of calculations, requisites, references, operating examples.

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

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REQUIREMENTS 49 Preliminary drawings sent to the customer shall include the following: construction and operating features; materials; weight; compression ratios; fluid levels at static, extended, and compressed positions; surface treatments; material strengths; and applicable specifications. Schematics shall include static, extended, and compressed positions of the nose and main wheels; angular relation of the shock absorber to the ground line (tail down and tail up); center-of-gravity positions and associated gross weights; and static wheel reactions at the landing gross weight (USAF/USN).

Navy Specification SD-24, "General Specification for Design and Construction of Aircraft Weapon Systems," Department of the Navy, Bureau of Naval Weapons. 4 REQUIREMENTS This chapter provides the designer with requirements relating to landing gear design. , size and placement of part numbers on wheels, their surface finish, or types of bearings. Also, the source of a requirement is not given whenever it is considered to be acceptable internationally and by both military and civil authorities. S.

55 MAC Frame a~ded and gear moved aft since abov location does not allow 15 deg angle with satisfactory tail-down angle e Use 12-15 deg initially -lr--'-" (LG at static) 15 d e g ~ STEP 6 Fig. 1 First steps in longitudinal location. INITIAL LAYOUT 27 department specializing in aircraft weight and balance and are based on negotiations with the Stability and Control Department. g. g. 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.

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