Calculation of the bending of electromechanical aircraft element made of the carbon fiber

Energy Management of Municipal Transportation Facilities and Transport - EMMFT 2017

Danilova-Volkovskaya, Galina^1 ; Chepurnenko, Anton^2 ; Begak, Aleksandr^1 ; Savchenko, Andrey^2

North-Caucasian Federal University, Ave 40 Let Oktyabrya, 56, Pyatigorsk

357500, Russia^1

Don State Technical University, Sotcialisticheskaya st., 162, Rostov-on-Don

344022, Russia^2

关键词: Aircraft elements;    Method of calculation;    Variable thickness;   

Others  :  https://iopscience.iop.org/article/10.1088/1755-1315/90/1/012046/pdf
DOI  :  10.1088/1755-1315/90/1/012046

来源: IOP

【 摘 要 】

We consider a method of calculation of an orthotropic plate with variable thickness. The solution is performed numerically by the finite element method. The calculation is made for the springs of a hang glider made of carbon fiber. The comparison of the results with Sofistik software complex is given.