It appears you don't have support to open PDFs in this web browser. To view this file, Open with your PDF reader
Abstract
The Boeing 747-400 aircraft incorporates a tricycle four-wheeled and two-axled landing gear. Being a jumbo-jet, the landing gear of Boeing 747-400 deals with tremendous loads during an approach, therefore, it becomes extremely important to identify critical sections and estimate the maximum stresses the gear can take, corresponding to various glideslopes. This paper deals with the determination of critical section and stresses developed in a landing gear during an approach. Three glideslopes of 3, 5 and 10 degrees were used to find critical section in a landing gear.
You have requested "on-the-fly" machine translation of selected content from our databases. This functionality is provided solely for your convenience and is in no way intended to replace human translation. Show full disclaimer
Neither ProQuest nor its licensors make any representations or warranties with respect to the translations. The translations are automatically generated "AS IS" and "AS AVAILABLE" and are not retained in our systems. PROQUEST AND ITS LICENSORS SPECIFICALLY DISCLAIM ANY AND ALL EXPRESS OR IMPLIED WARRANTIES, INCLUDING WITHOUT LIMITATION, ANY WARRANTIES FOR AVAILABILITY, ACCURACY, TIMELINESS, COMPLETENESS, NON-INFRINGMENT, MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE. Your use of the translations is subject to all use restrictions contained in your Electronic Products License Agreement and by using the translation functionality you agree to forgo any and all claims against ProQuest or its licensors for your use of the translation functionality and any output derived there from. Hide full disclaimer
Details
1 Associate Professor, Dept. of Mechanical Engineering, Dwarkadas J. Sanghvi College of Engineering, Mumbai, India
2 UG Student, Dept. of Mechanical Engineering, Dwarkadas J. Sanghvi College of Engineering, Mumbai, India