What is he best known for?
The fields of study he is best known for:
- Mechanics
- Fluid dynamics
- Boundary layer
His primary areas of investigation include Mechanics, Boundary layer, Classical mechanics, Navier–Stokes equations and Compressible flow.
His studies link Wavenumber with Mechanics.
The various areas that Hermann F. Fasel examines in his Boundary layer study include Computational fluid dynamics, Numerical analysis, Mathematical analysis and Vortex, Vorticity.
His studies deal with areas such as Reynolds-averaged Navier–Stokes equations, Turbulence, Large eddy simulation, Direct numerical simulation and Supersonic speed as well as Classical mechanics.
His Navier–Stokes equations study combines topics in areas such as Incompressible flow and Finite difference method.
His Mach number study incorporates themes from Hypersonic speed, Boundary and Nonlinear system.
His most cited work include:
- A high-order immersed interface method for simulating unsteady incompressible flows on irregular domains (261 citations)
- Evolution of three-dimensional coherent structures in a flat-plate boundary layer (213 citations)
- Investigation of the stability of boundary layers by a finite-difference model of the Navier—Stokes equations (212 citations)
What are the main themes of his work throughout his whole career to date?
Hermann F. Fasel spends much of his time researching Mechanics, Boundary layer, Turbulence, Laminar flow and Reynolds number.
Mechanics is frequently linked to Classical mechanics in his study.
Hermann F. Fasel focuses mostly in the field of Boundary layer, narrowing it down to matters related to Nonlinear system and, in some cases, Amplitude.
As part of the same scientific family, Hermann F. Fasel usually focuses on Turbulence, concentrating on Computational fluid dynamics and intersecting with Navier–Stokes equations and Incompressible flow.
His Laminar flow research focuses on subjects like Vortex generator, which are linked to Turbine.
His work carried out in the field of Reynolds number brings together such families of science as Turbine blade, Angle of attack, Airfoil, Simulation and Drag.
He most often published in these fields:
- Mechanics (74.33%)
- Boundary layer (35.22%)
- Turbulence (28.06%)
What were the highlights of his more recent work (between 2015-2021)?
- Mechanics (74.33%)
- Boundary layer (35.22%)
- Mach number (18.51%)
In recent papers he was focusing on the following fields of study:
Hermann F. Fasel mostly deals with Mechanics, Boundary layer, Mach number, Hypersonic speed and Cone.
His Mechanics study frequently intersects with other fields, such as Nonlinear system.
Hermann F. Fasel combines subjects such as Direct numerical simulation, Reynolds number and Supersonic speed with his study of Boundary layer.
His Mach number research is multidisciplinary, incorporating elements of Layer, Angle of attack and Optics, Wavenumber.
His Hypersonic speed study also includes
- Compressible navier stokes equations, Navier stokes, Navier–Stokes equations, Numerical analysis and Curvilinear coordinates most often made with reference to Jacobian matrix and determinant,
- Solver that intertwine with fields like Compressibility, Applied mathematics and System of linear equations,
- Mathematical analysis that connect with fields like Mathematical optimization.
In his research, Separation is intimately related to Turbulence, which falls under the overarching field of Laminar flow.
Between 2015 and 2021, his most popular works were:
- Direct numerical simulations of hypersonic boundary-layer transition for a flared cone: fundamental breakdown (37 citations)
- Towards simulating natural transition in hypersonic boundary layers via random inflow disturbances (30 citations)
- History and Progress of Boundary-Layer Transition on a Mach-6 Flared Cone (23 citations)
In his most recent research, the most cited papers focused on:
- Mechanics
- Fluid dynamics
- Thermodynamics
The scientist’s investigation covers issues in Mechanics, Boundary layer, Mach number, Hypersonic speed and Wave packet.
His study connects Amplitude and Mechanics.
His study in Boundary layer is interdisciplinary in nature, drawing from both Shock wave and Shock.
The concepts of his Mach number study are interwoven with issues in Angle of attack, Optics, Wavenumber and Cone.
His research in Angle of attack intersects with topics in Incompressible flow, Adverse pressure gradient, Computational fluid dynamics and Vortex.
His Hypersonic speed research includes elements of Supersonic speed and Nonlinear system.
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