Wei Huang

Research.com Recognitions

• 2018 - OSA Fellows Wei Huang Northwestern Polytechnical Univ. & Nanjing Tech Univ., China For pioneering leadership in organic optoelectronics which developed from physics, chemistry, materials, electronics, and information science & technology based interdisciplines.

Overview

Best Publications

• Influences of the turbulence model and the slot width on the transverse slot injection flow field in supersonic flows

  Wei Huang;Wei-dong Liu;Shi-bin Li;Zhi-xun Xia

  482
  Citations

• Transverse jet in supersonic crossflows

  Wei Huang

  366
  Citations

• Numerical investigation on the ram–scram transition mechanism in a strut-based dual-mode scramjet combustor

  Wei Huang;Li Yan

  261
  Citations

• Recent advances in cavity-based scramjet engine- a brief review

  Gautam Choubey;Yuvarajan Devarajan;Wei Huang;Kulmani Mehar

  260
  Citations

• Supersonic mixing in airbreathing propulsion systems for hypersonic flights

  Wei Huang;Zhao-bo Du;Li Yan;Zhi-xun Xia

  258
  Citations

• Survey on the mode transition technique in combined cycle propulsion systems

  Wei Huang;Li Yan;Jian-guo Tan

  249
  Citations

• Detailed parametric investigations on drag and heat flux reduction induced by a combinational spike and opposing jet concept in hypersonic flows

  Min Ou;Li Yan;Wei Huang;Shi-bin Li

  229
  Citations

• Flame propagation and stabilization in dual-mode scramjet combustors: A survey

  Wei Huang;Zhao-bo Du;Li Yan;R. Moradi

  220
  Citations

• Performance evaluation and parametric analysis on cantilevered ramp injector in supersonic flows

  Wei Huang;Shi-bin Li;Li Yan;Zhen-guo Wang

  220
  Citations

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

  Wei Huang

  206
  Citations

• Hydrogen fuel in scramjet engines - A brief review

  Gautam Choubey;Yuvarajan D;Wei Huang;Li Yan

  197
  Citations

• Recent advances in the shock wave/boundary layer interaction and its control in internal and external flows

  Wei Huang;Han Wu;Yan-guang Yang;Li Yan

  193
  Citations

• A survey on numerical simulations of drag and heat reduction mechanism in supersonic/hypersonic flows

  Xiwan Sun;Wei Huang;Min Ou;Ruirui Zhang

  172
  Citations

• Experimental investigation on drag and heat flux reduction in supersonic/hypersonic flows: A survey

  Zhen-guo Wang;Xi-wan Sun;Wei Huang;Shi-bin Li

  169
  Citations

• Numerical investigation on the shock wave transition in a three-dimensional scramjet isolator

  Wei Huang;Wei Huang;Zhen-guo Wang;Mohamed Pourkashanian;Lin Ma

  169
  Citations

• Mixing enhancement strategies and their mechanisms in supersonic flows: A brief review

  Wei Huang

  168
  Citations

• Drag and heat flux reduction mechanism induced by the spike and its combinations in supersonic flows: A review

  Wei Huang;Zheng Chen;Li Yan;Bin-bin Yan

  163
  Citations

• Mixing augmentation induced by the interaction between the oblique shock wave and a sonic hydrogen jet in supersonic flows

  Wei Huang;Jian-guo Tan;Jun Liu;Li Yan

  150
  Citations

• Drag and heat reduction mechanism in the combinational opposing jet and acoustic cavity concept for hypersonic vehicles

  Wei Huang;Li Yan;Jun Liu;Liang Jin

  139
  Citations

• Recent research progress on transverse injection technique for scramjet applications-a brief review

  Gautam Choubey;Devarajan Yuvarajan;Wei Huang;Ahmad Shafee

  136
  Citations

• Parametric effects on the combustion flow field of a typical strut-based scramjet combustor

  Wei Huang;Wei Huang;ZhenGuo Wang;ShiBin Luo;Jun Liu

  134
  Citations

• Drag reduction mechanism induced by a combinational opposing jet and spike concept in supersonic flows

  Wei Huang;Jun Liu;Zhi-xun Xia

  125
  Citations