scispace - formally typeset
W

Wei Huang

Researcher at National University of Defense Technology

Publications -  167
Citations -  6484

Wei Huang is an academic researcher from National University of Defense Technology. The author has contributed to research in topics: Supersonic speed & Hypersonic speed. The author has an hindex of 38, co-authored 151 publications receiving 4561 citations.

Papers
More filters
Journal ArticleDOI

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

TL;DR: In this article, the effect of the turbulence model and slot width on the transverse slot injection flow field has been investigated numerically based on the grid independency analysis, and the predicted results have been compared with the experimental data available in the open literature.
Journal ArticleDOI

Transverse jet in supersonic crossflows

TL;DR: In this article, the transverse jet in supersonic crossflows has been summarized systematically from four aspects, namely single injection, multiport injection, interaction between jet and vortex generator, and interaction between the jet and shock wave.
Journal ArticleDOI

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

TL;DR: In this paper, the inlet boundary conditions at the entrance of the isolator and the jet-to-crossflow pressure ratio both have a large impact on the Ram-To-Scram mode transition.
Journal ArticleDOI

Survey on the mode transition technique in combined cycle propulsion systems

TL;DR: In this article, the research status on the mode transition of the combined cycle engines has been reviewed in detail, and three typical mode transition processes have been summarized, namely the ejector/ramjet mode transition for the rocket-based combined cycle engine, the turbojet/ramjets mode transition and the ramjet/scramjet phase transition.
Journal ArticleDOI

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

TL;DR: In this article, the effect of the swept angle, the ramp angle and the length of the step on the performance of the cantilevered ramp injector has been investigated numerically, and the predicted injectant mole fraction and static pressure profiles have been compared with the available experimental data in the open literature.