What is he best known for?
The fields of study he is best known for:
- Mechanics
- Thermodynamics
- Fluid dynamics
His main research concerns Mechanics, Turbulence, Reynolds number, Vortex and Boundary layer.
As a member of one scientific family, Wolfgang Schröder mostly works in the field of Mechanics, focusing on Classical mechanics and, on occasion, Reynolds stress.
His Turbulence study integrates concerns from other disciplines, such as Shear flow, Geometry, SPHERES and Fluid mechanics.
Wolfgang Schröder has included themes like Airfoil, Pipe flow, Bubble and Velocimetry in his Reynolds number study.
Wolfgang Schröder interconnects Flow separation, Mean flow and Vortex shedding in the investigation of issues within Vortex.
His Boundary layer research integrates issues from Jet and Meteorology.
His most cited work include:
- Acoustic perturbation equations based on flow decomposition via source filtering (422 citations)
- A comparison of second- and sixth-order methods for large-eddy simulations (227 citations)
- On the simulation of trailing edge noise with a hybrid LES/APE method (139 citations)
What are the main themes of his work throughout his whole career to date?
His scientific interests lie mostly in Mechanics, Turbulence, Reynolds number, Boundary layer and Vortex.
The study of Mechanics is intertwined with the study of Classical mechanics in a number of ways.
His work in Turbulence addresses subjects such as Trailing edge, which are connected to disciplines such as Acoustics.
His research investigates the connection between Reynolds number and topics such as Particle image velocimetry that intersect with problems in Optics.
His work deals with themes such as Wake and Inflow, which intersect with Vortex.
His Mach number research incorporates elements of Transonic, Shock wave, Shock, Freestream and Supersonic speed.
He most often published in these fields:
- Mechanics (67.80%)
- Turbulence (39.71%)
- Reynolds number (25.04%)
What were the highlights of his more recent work (between 2018-2021)?
- Mechanics (67.80%)
- Turbulence (39.71%)
- Reynolds number (25.04%)
In recent papers he was focusing on the following fields of study:
Wolfgang Schröder spends much of his time researching Mechanics, Turbulence, Reynolds number, Drag and Boundary layer.
Mechanics is closely attributed to Amplitude in his research.
His studies in Turbulence integrate themes in fields like Airfoil and Isotropy.
His Reynolds number research includes themes of Flow separation and Stress.
His Drag study combines topics in areas such as Surface wave, Reduction and Vorticity.
The Boundary layer thickness research Wolfgang Schröder does as part of his general Boundary layer study is frequently linked to other disciplines of science, such as Population, therefore creating a link between diverse domains of science.
Between 2018 and 2021, his most popular works were:
- Analysis of tip-leakage flow in an axial fan at varying tip-gap sizes and operating conditions (19 citations)
- Analysis of tip-leakage flow in an axial fan at varying tip-gap sizes and operating conditions (19 citations)
- The Effect of Postoperative Complications After Minimally Invasive Esophagectomy on Long-term Survival: An International Multicenter Cohort Study. (17 citations)
In his most recent research, the most cited papers focused on:
- Mechanics
- Thermodynamics
- Fluid dynamics
Mechanics, Reynolds number, Turbulence, Drag and Boundary layer are his primary areas of study.
His research in Mechanics intersects with topics in Turbine and Computational aeroacoustics.
The various areas that Wolfgang Schröder examines in his Reynolds number study include Probability density function, Mach number, Shear stress, Flow separation and Vortex.
The study incorporates disciplines such as Isotropy, Dissipation, Kinetic energy and Interpolation in addition to Turbulence.
His research in Drag focuses on subjects like Lift, which are connected to Adverse pressure gradient, Airfoil, Vorticity, External flow and Potential flow.
His Boundary layer research focuses on Surface wave and how it connects with Boundary layer thickness.
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