Hostname: page-component-cd9895bd7-dzt6s Total loading time: 0 Render date: 2024-12-22T16:47:05.951Z Has data issue: false hasContentIssue false

Theory of Aircraft Undercarriages in Relation to Absorption of Initial Landing Impact

Published online by Cambridge University Press:  28 July 2016

Extract

Many complex machines and mechanical systems have an ideal and abstract form which has been evolved from fundamental theory without reference to those engineering principles that are so essential in practice. Thus the heat engine has its Carnot cycle and the propeller its actuator disc. With these, and numerous other examples, the object is to provide a standard of reference, to give an ideal which can be approached but never reached and, most important, to indicate the fundamental limitations imposed by theory and prevent profitless investigations.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1942

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)