Abstract
In the modern aviation industry, the task of increasing the structural strength of the aircraft wing is being actualize. The author presents an engineering methodology for power calculation and design of composite aircraft structures based on the analysis of strength characteristics of metal and metal-polymer composite materials. The paper uses theoretical and empirical research methods, as well as the results of foreign and domestic scientific materials.
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Published version (
Free)
Free) 
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
