The design of aircraft landing gear / R. Kyle Schmidt.

Saved in:
Bibliographic Details
Online Access: Full Text (via Knovel)
Main Author: Schmidt, R. Kyle (Author)
Format: eBook
Language:English
Published: Warrendale, Pennsylvania, USA : SAE International, [2020]
Subjects:

MARC

LEADER 00000cam a2200000xi 4500
001 b12078282
003 CoU
005 20220128044102.0
006 m o d
007 cr |||||||||||
008 210706s2020 paua ob 001 0 eng d
019 |a 1273206175 
020 |a 9780768099430  |q (electronic bk.) 
020 |a 0768099439  |q (electronic bk.) 
020 |z 0768099420 
020 |z 9780768099423 
020 |a 9780768083453  |q (electronic bk.) 
020 |a 0768083451  |q (electronic bk.) 
024 7 |a 10.4271/9780768099430 
035 |a (OCoLC)kno1259287650 
035 |a (OCoLC)1259287650  |z (OCoLC)1273206175 
040 |a IEEEE  |b eng  |e rda  |e pn  |c IEEEE  |d OCLCO  |d YDX  |d N$T 
049 |a GWRE 
050 4 |a TL682  |b .S36 2020eb 
100 1 |a Schmidt, R. Kyle,  |e author.  |0 http://id.loc.gov/authorities/names/nb2015024900. 
245 1 4 |a The design of aircraft landing gear /  |c R. Kyle Schmidt. 
264 1 |a Warrendale, Pennsylvania, USA :  |b SAE International,  |c [2020] 
300 |a 1 online resource (2 volumes (xxiii, 1,049, 16 pages)) :  |b illustrations (some color) 
336 |a text  |b txt  |2 rdacontent. 
337 |a computer  |b c  |2 rdamedia. 
338 |a online resource  |b cr  |2 rdacarrier. 
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 Description based on print version record. 
650 0 |a Airplanes  |x Landing gear  |x Design and construction. 
650 7 |a Airplanes  |x Landing gear  |x Design and construction.  |2 fast  |0 (OCoLC)fst00803264. 
776 0 8 |i Print version:  |a Schmidt, R. Kyle.  |t Design of aircraft landing gear.  |d Warrendale, Pennsylvania, USA : SAE International, [2020]  |z 0768099420  |w (OCoLC)1253292096. 
856 4 0 |u https://colorado.idm.oclc.org/login?url=https://app.knovel.com/hotlink/toc/id:kpDALGV001/design-of-aircraft?kpromoter=marc  |z Full Text (via Knovel) 
907 |a .b120782820  |b 03-01-22  |c 02-03-22 
998 |a web  |b 02-28-22  |c b  |d b   |e -  |f eng  |g pau  |h 4  |i 1 
907 |a .b120782820  |b 02-28-22  |c 02-03-22 
944 |a MARS - RDA ENRICHED 
915 |a I 
956 |a Knovel 
956 |b ACADEMIC - Aerospace & Radar Technology 
956 |b ACADEMIC - Mechanics & Mechanical Engineering 
999 f f |i e36380b7-7db0-559d-8e32-a6e7c3474003  |s ec183ba3-8a6b-5339-8892-817a99b90a17 
952 f f |p Can circulate  |a University of Colorado Boulder  |b Online  |c Online  |d Online  |e TL682 .S36 2020eb  |h Library of Congress classification  |i web  |n 1