What is he best known for?
The fields of study he is best known for:
- Mechanical engineering
- Mechanics
- Thermodynamics
His primary scientific interests are in Mechanics, Supersonic speed, Materials science, Aerospace engineering and Combustor.
His work on Turbulence as part of general Mechanics study is frequently linked to Overall pressure ratio, bridging the gap between disciplines.
Wei Huang interconnects Transverse plane, Jet, Drag and Injector in the investigation of issues within Supersonic speed.
His study in Hypersonic speed and Propulsion falls under the purview of Aerospace engineering.
In general Combustor study, his work on Scramjet often relates to the realm of Shock wave, thereby connecting several areas of interest.
His work focuses on many connections between Choked flow and other disciplines, such as Mach number, that overlap with his field of interest in Freestream.
His most cited work include:
- Influences of the turbulence model and the slot width on the transverse slot injection flow field in supersonic flows (238 citations)
- Transverse jet in supersonic crossflows (138 citations)
- Numerical investigation on the ram–scram transition mechanism in a strut-based dual-mode scramjet combustor (122 citations)
What are the main themes of his work throughout his whole career to date?
His primary areas of study are Mechanics, Materials science, Hypersonic speed, Supersonic speed and Aerospace engineering.
His Turbulence, Jet, Drag, Choked flow and Mach number study are his primary interests in Mechanics.
His work carried out in the field of Drag brings together such families of science as Classical mechanics and Heat flux.
His Hypersonic speed research is multidisciplinary, incorporating elements of Lift-to-drag ratio, Aerodynamics, Leading edge and Inlet.
He has included themes like Optics, Mechanical engineering, Injector and Vortex, Vortex generator in his Supersonic speed study.
The Range, Propulsion and Airframe research Wei Huang does as part of his general Aerospace engineering study is frequently linked to other disciplines of science, such as Scramjet and Combustor, therefore creating a link between diverse domains of science.
He most often published in these fields:
- Mechanics (59.03%)
- Materials science (36.81%)
- Hypersonic speed (34.72%)
What were the highlights of his more recent work (between 2019-2021)?
- Mechanics (59.03%)
- Mach number (27.08%)
- Supersonic speed (34.72%)
In recent papers he was focusing on the following fields of study:
Wei Huang mainly investigates Mechanics, Mach number, Supersonic speed, Shock wave and Materials science.
His research on Mechanics often connects related areas such as Head.
His study in Mach number is interdisciplinary in nature, drawing from both Hypersonic speed and Wind tunnel.
His study ties his expertise on Aerodynamics together with the subject of Supersonic speed.
His biological study spans a wide range of topics, including Turbulence and Boundary layer.
He combines subjects such as Freestream and Shock with his study of Drag.
Between 2019 and 2021, his most popular works were:
- Hydrogen fuel in scramjet engines - A brief review (22 citations)
- Recent advances in the shock wave/boundary layer interaction and its control in internal and external flows (14 citations)
- Shock wave/turbulence boundary layer interaction control with the secondary recirculation jet in a supersonic flow (9 citations)
In his most recent research, the most cited papers focused on:
- Mechanical engineering
- Thermodynamics
- Mechanics
Wei Huang mainly focuses on Mach number, Aerospace engineering, Hypersonic flight, Range and Propulsion.
The study incorporates disciplines such as Hypersonic speed, External flow, Aerodynamics and Wind tunnel in addition to Mach number.
Wei Huang is involved in the study of Aerospace engineering that focuses on Supersonic speed in particular.
His Supersonic speed study combines topics from a wide range of disciplines, such as Flight envelope and Downwash.
His Hypersonic flight study combines topics in areas such as Shock wave, Boundary value problem, Internal flow and Boundary layer.
The concepts of his Propulsion study are interwoven with issues in Transverse plane and Total pressure.
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