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The design of aircraft landing gear

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	The design of aircraft landing gear / by Robert Kyle Schmidt.
作者:	Schmidt, Robert Kyle,,
面頁冊數:	1 online resource (1 PDF (1,090 pages)) :illustrations. :
標題:	Astronautics. -
ISBN:	9780768099430

The design of aircraft landing gear
Schmidt, Robert Kyle,,

The design of aircraft landing gear [electronic resource] /by Robert Kyle Schmidt. - 1 online resource (1 PDF (1,090 pages)) :illustrations. - Society of Automotive Engineers. Electronic publications. - Society of Automotive Engineers..

Includes bibliographical references and index.

The Design of Aircraft Landing Gear is designed to guide the reader through the key principles of landing system design and to provide additional references when available. Many problems which must be confronted have already been addressed by others in the past, but the information is not known or shared, leading to the observation that there are few new problems, but many new people. It is intended to share much of the existing information and provide avenues for further exploration. The design of an aircraft and its associated systems, including the landing system, involves iterative loops as the impact of each modification to a system or component is evaluated against the whole. It is rare to find that the lightest possible landing gear represents the best solution for the aircraft: the lightest landing gear may require attachment structures which don't exist and which would require significant weight and compromise on the part of the airframe structure design.

ISBN: 9780768099430

Standard No.: 10.4271/9780768099430doiSubjects--Topical Terms:

646219
Astronautics.
Index Terms--Genre/Form:

554714
Electronic books.

LC Class. No.: TL682 / .S36 2021eb

Dewey Class. No.: 629.134/381

The design of aircraft landing gear
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035 $a (OCoLC)1250636206
035 $a (CaBNVSL)slc00001463
035 $a R-455
035 $a 9780768099430
040 $a CaBNVSL $b eng $e rda $c CaBNVSL $d CaBNVSL $d UtOrBLW
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100 1 $a Schmidt, Robert Kyle,, $e author. $3 1484192
245 1 4 $a The design of aircraft landing gear $h [electronic resource] / $c by Robert Kyle Schmidt.
264 1 $a Warrendale, Pa. (400 Commonwealth Dr., Warrendale PA USA) : $b Society of Automotive Engineers, $c 2021.
300 $a 1 online resource (1 PDF (1,090 pages)) : $b illustrations.
336 $a text $b txt $2 rdacontent
337 $a computer $b c $2 rdamedia
338 $a online resource $b cr $2 rdacarrier
490 1 $a Society of Automotive Engineers. Electronic publications
504 $a Includes bibliographical references and index.
520 3 $a The Design of Aircraft Landing Gear is designed to guide the reader through the key principles of landing system design and to provide additional references when available. Many problems which must be confronted have already been addressed by others in the past, but the information is not known or shared, leading to the observation that there are few new problems, but many new people. It is intended to share much of the existing information and provide avenues for further exploration. The design of an aircraft and its associated systems, including the landing system, involves iterative loops as the impact of each modification to a system or component is evaluated against the whole. It is rare to find that the lightest possible landing gear represents the best solution for the aircraft: the lightest landing gear may require attachment structures which don't exist and which would require significant weight and compromise on the part of the airframe structure design.
588 $a Title from PDF title page (SAE Web site, 05/07/2021)
650 7 $a Astronautics. $3 646219
650 7 $a Aerospace and aviation technology. $2 thema $3 1484194
650 7 $a TECHNOLOGY & ENGINEERING / Aeronautics & Astronautics. $2 bisacsh $3 1413296
650 0 $a Airplanes $x Landing gear $x Design and construction. $3 1484193
655 0 $a Electronic books. $2 local $3 554714
710 2 $a Society of Automotive Engineers, $e issuing body. $3 1218618
776 0 8 $i Print version: $z 9780768099423
810 2 $a Society of Automotive Engineers. $3 639463
856 $3 SAE International $g https://doi.org/10.4271/9780768099430