Zobrazeno 1 - 10
of 39
pro vyhledávání: '"Xiao-yan Tong"'
Publikováno v:
International Journal of Aerospace Engineering, Vol 2021 (2021)
The size of aircraft models that can be tested in icing wind tunnels is limited by the dimensions of the facilities in present; it is an effective method to replace the large model with a hybrid airfoil to carry out the experiment. A design method of
Externí odkaz:
https://doaj.org/article/695ca1c3769f49e7b6b0dda5d16babb2
Publikováno v:
Guoji Yanke Zazhi, Vol 15, Iss 5, Pp 767-771 (2015)
AIM: To observe the expression of Acin1(apoptotic chromatin condensation inducer 1)in congenital cataract mouse retina during development and investigate the differences of retinal apoptosis and the connection of lens and retina development between c
Externí odkaz:
https://doaj.org/article/a95f2b85e39945799b313c7a899c4d8b
Autor:
Xin, Liu, Lian-Hui, Wang, Zi-Heng, Xu, Jin, Shu, Meng-Yuan, Dong, Xiao-Yan, Tong, Xiu-Yun, Xu
Publikováno v:
Zhongguo shi yan xue ye xue za zhi. 30(6)
To explore the molecular biology of D variant blood group withA total of 6 samples from 3 generations of a family were analyzed. RHD blood group was identified by saline test tube and microcolumn gel card method. 10 exons ofThe proband was identified
Publikováno v:
Applied Mechanics and Materials. 607:409-412
Finite element model of folding wings was designed in the light of structural scheme, and each part of the model used composites. Different aeroelastic analysis models were built from emission to cruise, and then the models were made the study focus
Publikováno v:
Applied Mechanics and Materials. 443:129-133
To simulate the impact response of the moving body in the permanent magnetic actuator, this paper takes the magnetic force of the moving body at different positions as one of the input loads for the impact simulation, which avoids the coupling calcul
Publikováno v:
Applied Mechanics and Materials. :410-414
Folding wings of UAV may lead to high bending and torsion deformation under flight load. In order to solve the problem, an improved folding wing mechanism is proposed, which makes support mechanism stiffness become enough big. By means of CATIA and A
Publikováno v:
Advanced Materials Research. :764-767
An experimental study was carried out to study the low-velocity impact characteristics and the influence of impact energy on the damage of plain woven carbon fiber reinforced silicon carbide composite. Visual, ultrasonic scanning, X-ray, industrial C
Publikováno v:
Advanced Materials Research. 548:461-464
In the light of growing global competition, organizations around the world today are constantly under pressure to produce high-quality products at an economical price. The integration of design and manufacturing activities into one common engineering
Publikováno v:
Advanced Materials Research. 502:56-59
The aim of this paper is to study the influence of manufacturing defects on coefficient of thermal expansion (CTE) of Plain Weave C/SiC by using the finite element computational micromechanics (FECM) method. Utilizing photomicrographs taken by scanni
Publikováno v:
Advanced Materials Research. 460:342-346
Utilized photomicrographs taken by scanning electron microscope (SEM), an accurate representative volume element (RVE) model for plain weave C/SiC composites is established. Based on the steady-analysis method, the in-plane and thickness direction th