Redirigiendo al acceso original de articulo en 19 segundos...
Inicio  /  Applied Sciences  /  Vol: 10 Par: 23 (2020)  /  Artículo
ARTÍCULO
TITULO

Finite Element Analysis and Investigation on Spinning of Quadrilateral Parts with Hollow Cross-Sections Based on Hypocycloid Theory

Xibin Ou    
Xianyong Zhu    
Peng Gu    
Baichao Wang    
Jing Li    
Xia Liu    
Chuang Liu    
Fei He and Qiang Li    

Resumen

Authors are encouraged to provide a concise description of the specific application or a potential application of the work. This section is not mandatory.

 Artículos similares

       
 
Cesare Patuelli, Enrico Cestino and Giacomo Frulla    
Vibration analysis of wing-box structures is a crucial aspect of the aeronautic design to avoid aeroelastic effects during normal flight operations. The deformation of a wing structure can induce nonlinear couplings, causing a different dynamic behavior ... ver más
Revista: Aerospace

 
Xingxing Huang, Kang Han, Zhenyu Lu, Shuncheng Zhang and Liang Guo    
In order to reduce the influence of temperature deformation of large-size body-mounted radiators on the observation accuracy of space station telescopes and adapt to launch vibration loads, this paper proposes a floating combination stress release mechan... ver más
Revista: Aerospace

 
George Tzoumakis, Konstantinos Fotopoulos and George Lampeas    
Future liquid hydrogen-powered aircraft requires the design and optimization of a large number of systems and subsystems, with cryogenic tanks being one of the largest and most critical. Considering previous space applications, these tanks are usually st... ver más
Revista: Aerospace

 
Grigorios Kostopoulos, Konstantinos Stamoulis, Vaios Lappas and Stelios K. Georgantzinos    
This study explores the shape-morphing behavior of 4D-printed structures made from Polylactic Acid (PLA), a prominent bio-sourced shape-memory polymer. Focusing on the response of these structures to thermal stimuli, this research investigates how variou... ver más
Revista: Aerospace

 
Long Li, Yiming Peng, Yifeng Wang, Xiaohui Wei and Hong Nie    
Arresting gear systems play a vital role in carrier-based aircraft landing. In order to accurately understand the process of arresting hook and cable, this study introduces a parameter inversion method to model the arresting cable and applies it to the t... ver más
Revista: Aerospace