Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Bao Qi Liu"'
Autor:
Fei-Fei Luo, Jing Wang, Zhan-Fei Zhang, Si-Ting Lin, Tie-Jun Huang, Bao-Qi Liu, Mei-Ling Fan, Li-Xia Peng, Shu-Tao Zheng, Chang-Fu Yang, Bi-Jun Huang
Publikováno v:
Frontiers in Bioscience-Landmark, Vol 28, Iss 9, p 212 (2023)
Background: Esophageal squamous cell carcinoma (ESCC) is a highly lethal tumor type, but studies on the ESCC tumor microenvironment are limited. We found that cystatin SN (CST1) plays an important role in the ESCC tumor microenvironment. CST1 has bee
Externí odkaz:
https://doaj.org/article/f23ecff9507a4150b1a67bfd2075cdbc
Autor:
Jin Luo, Qiu-Xia Chen, Pan Li, Zhi-Ming Yang, He Yu, Bao-Qi Liu, Mei-Ling Fan, Zhuo-Mao Mo, Yong-Dan Wang, Mei-Ling Zhou, Hao Hu, Ling Yu, Bi-Jun Huang, Shi-jun Zhang
Background Hepatocellular carcinoma (HCC), a common type of cancer, has a strong metastatic ability and poor prognosis. The tumor microenvironment is the “soil” for the occurrence and development of tumors, with exosomes playing an important role
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e9dfac324e83f314affaff3a8daff21f
https://doi.org/10.21203/rs.3.rs-2266609/v1
https://doi.org/10.21203/rs.3.rs-2266609/v1
Autor:
Jing Wang, Tie-Jun Huang, Yan Mei, Fei-Fei Luo, De-Huan Xie, Li-Xia Peng, Bao-Qi Liu, Mei-Ling Fan, Jiang-Bo Zhang, Shu-Tao Zheng, Chao-Nan Qian, Bi-Jun Huang
Publikováno v:
Cancer gene therapy.
Esophageal squamous cell carcinoma (ESCC) is one of the most common malignant tumors in China. However, there are no targets to treat ESCC because the molecular mechanism behind the cancer is still unclear. Here, we found a novel long noncoding RNA L
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5129241ea6050db9fc4d9e9ce41c47c2
https://pubmed.ncbi.nlm.nih.gov/36357564
https://pubmed.ncbi.nlm.nih.gov/36357564
Publikováno v:
Journal of Aircraft. 50:879-885
Crack paths in friction stir-welded 2198-T8 SE(T) plates with pad-up are investigated. Fatigue tests are performed with and without a friction stir weld in a range of samples, and crack paths and fatigue crack growth rates are compared. The effects o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::abbd0cdd0cf65e640b4c1056a8f93dbe
https://doi.org/10.2514/1.c032016
https://doi.org/10.2514/1.c032016
Publikováno v:
Applied Mechanics and Materials. :651-656
Al-Li alloy 2198-T8 was used in the fuselage application. Integral fuselage panels were joined by double friction stir welds. Fatigue tests were conducted in the R=0.1. Notch was made between two welds. Residual stresses were measured and analyzed in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d2810262c4c14fd6ab61b7eedce760b3
https://doi.org/10.4028/www.scientific.net/amm.138-139.651
https://doi.org/10.4028/www.scientific.net/amm.138-139.651
Residual Stress Effects on Crack Growth in Nugget of Al-Li Alloy 2195-T8 Friction Stir Welded Joints
Publikováno v:
Applied Mechanics and Materials. :646-650
In this work, Compact-Tension (C(T)) specimens with transverse welds in the sample centre were designed. The residual stress distributions were measured parallel and perpendicular to the weld nugget. Fatigue crack growth (FCG) rates were measured in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d440168e52e6c67c2239443f12b78283
https://doi.org/10.4028/www.scientific.net/amm.138-139.646
https://doi.org/10.4028/www.scientific.net/amm.138-139.646
Publikováno v:
Advanced Materials Research. :1135-1140
To improve damage tolerance performance, GLARE was used as bonded crack retarders in this paper. Fatigue tests were run with unbonded and bonded samples; then test results between them was compared. Thermal residual stresses had been studied. It was
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a091defc21c9ff6fcd1b4e1ae388968f
https://doi.org/10.4028/www.scientific.net/amr.217-218.1135
https://doi.org/10.4028/www.scientific.net/amr.217-218.1135
Publikováno v:
Journal of Aircraft. May/Jun2013, Vol. 50 Issue 3, p879-885. 7p.