Engineering topics
Wei, Hong
Publications and source records attributed to Wei, Hong.
Circular RNA circZFR contributes to papillary thyroid cancer cell proliferation and invasion by sponging miR-1261 and facilitating C8orf4 expression
In recent years, more and more circular RNAs (circRNAs) have been identified in multiple tissues and cells. Increasing evidences show circRNAs play important roles in human cancers. However, the role of circRNAs in papillary thyroid carcinoma (PTC) remains largely unknown. In this study, we identified a new circRNA circZFR that was significantly upregulated in PTC tissues compared to adjacent normal tissues. Furthermore, circZFR expression level was negatively correlated with clinical severity. We found that circZFR knockdown dramatically inhibited the proliferation, migration and invasion of PTC cells in vitro. Mechanistically, we found circZFR could promote C8orf4 expression via serving as a competing endogenous RNA (ceRNA) of miR-1261 in PTC cells. Rescue assays indicated that restoration of C8orf4 significantly attenuated the inhibitory effects of circZFR knockdown on PTC cell proliferation, migration and invasion. In summary, our findings demonstrated that circRNA circZFR exerted oncogenic roles via regulating miR-1261/C8orf4 axis in PTC, which suggested circZFR might be a potential therapeutic target.
Protein arginine methyltransferase 1 coordinates the epithelial-mesenchymal transition/proliferation dichotomy in gastric cancer cells
Protein arginine methyltransferase 1 (PRMT1) is up-regulated and promotes migration, invasion and proliferation in wide range of cancers. However, we for the first time identify that PRMT1 promotes migration and invasion and inhibits proliferation in gastric cancer cells, a phenomenon called “migration-proliferation dichotomy”. First, we find that PRMT1 overexpression promotes migration and invasion and inhibits proliferation, whereas PRMT1 knockdown reverses the above abilities. Next, PRMT1 reduces the expression of epithelial marker E-cadherin and increases the expression of mesenchymal markers including N-cadherin, Vimentin, snail and β-catenin in gastric cancer cells. Furthermore, our studies show that PRMT1 silencing promotes the phosphorylation of LATS1, and then induces YAP phosphorylation, while overexpression of PRMT1 down-regulates the phosphorylation of LATS1 and YAP, indicating that PRMT1 inhibits EMT probably via Hippo signaling. Collectively, the present study reveals important roles of PRMT1 in progression of gastric cancer. Given the dual functions of PRMT1, it is as a potential drug target of gastric cancer with extreme caution.
Laser Lightcraft Performance
The purpose of this study is to establish the technical ground for modeling the physics of laser powered pulse detonation phenomenon. The principle of the laser power propulsion is that when high-powered laser is focused at a small area near the surface of a thruster, the intense energy causes the electrical breakdown of the working fluid (e.g. air) and forming high speed plasma (known as the inverse Bremsstrahlung, IB, effect). The intense heat and high pressure created in the plasma consequently causes the surrounding to heat up and expand until the thrust producing shock waves are formed. This complex process of gas ionization, increase in radiation absorption and the forming of plasma and shock waves will be investigated in the development of the present numerical model. In the first phase of this study, laser light focusing, radiation absorption and shock wave propagation over the entire pulsed cycle are modeled. The model geometry and test conditions of known benchmark experiments such as those in Myrabo's experiment will be employed in the numerical model validation simulations. The calculated performance data will be compared to the test data.
Injector Design Tool Improvements: User's manual for FDNS V.4.5
The major emphasis of the current effort is in the development and validation of an efficient parallel machine computational model, based on the FDNS code, to analyze the fluid dynamics of a wide variety of liquid jet configurations for general liquid rocket engine injection system applications. This model includes physical models for droplet atomization, breakup/coalescence, evaporation, turbulence mixing and gas-phase combustion. Benchmark validation cases for liquid rocket engine chamber combustion conditions will be performed for model validation purpose. Test cases may include shear coaxial, swirl coaxial and impinging injection systems with combinations LOXIH2 or LOXISP-1 propellant injector elements used in rocket engine designs. As a final goal of this project, a well tested parallel CFD performance methodology together with a user's operation description in a final technical report will be reported at the end of the proposed research effort.