Design exploration of three-dimensional transverse jet in a supersonic crossflow based on data mining and multi-objective design optimization approaches

By Wei Huang. 2014

152 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/78a99c58418416d5b6a33d3e8f94021b20966b8f

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Li Yan
2. Tian-tian Zhang
3. Zhenguo Wang
4. Wei Huang

In Computational Mechanics

1. Li Yan
2. Tian-tian Zhang
3. Zhenguo Wang
4. Wei Huang

Citations in the corpus

• A study of airfoil parameterization, modeling, and optimization based on the computational fluid dynamics method (2016, methodology): “, 2015), in addition to turbulent diffusion combustion in supersonic flows (Huang et al., 2012a). The equations are solved using a pressure-based (coupled) double-precision solver in Fluent Inc. (2006), and a second upwind scheme is applied to the convection terms.”
• Winglet design for vertical axis wind turbines based on a design of experiment and CFD approach (2019, background): “Ltip Rcant っcant 渇sweep けtip j SSW 0.003655 0.003743 0.003780 0.003643 0.003781 0.000855 SSB 0.000237 0.000149 0.000112 0.000249 0.000110 0.003036 DoFW 20 20 20 20 20 20 DoFB 4 4 4 4 4 4 Fvalue 0.3236 0.1985 0.1475 0.3411 0.1455 17.7505 F0.”