Abstract

Currently, significant interest among the developers of navigation devices, particularly dynamically tuned gyros, is caused by the design of elastic elements with specified properties. In turn, the development of optimal designs of elastic elements that provide the necessary rigidity of an airplane wing is of significant relevance. At the same time, if optimization is carried out, for example, within the framework of the conceptual design stage, which allows of certain simplifications, then it is advisable to apply its idealized core structure to correctly reproduce the most significant features of the wing frame powerwork.

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.