What is he best known for?
The fields of study he is best known for:
- Mechanics
- Quantum mechanics
- Fluid dynamics
His scientific interests lie mostly in Mechanics, Turbulence, Classical mechanics, Boundary layer and Direct numerical simulation.
Neil D. Sandham regularly links together related areas like Optics in his Mechanics studies.
In his study, Finite thickness and NACA airfoil is inextricably linked to Sound pressure, which falls within the broad field of Turbulence.
The Boundary layer study combines topics in areas such as Oblique shock, Shock wave and Shock.
The various areas that he examines in his Direct numerical simulation study include Trailing edge, Turbulence modeling, Boundary value problem and Aeroacoustics.
His Mach number research incorporates themes from Hypersonic speed, Meteorology and Instability.
His most cited work include:
- Low-Dissipative High-Order Shock-Capturing Methods Using Characteristic-Based Filters (491 citations)
- Direct numerical simulation of'short' laminar separation bubbles with turbulent reattachment (367 citations)
- Large-eddy simulation of low-frequency unsteadiness in a turbulent shock-induced separation bubble (330 citations)
What are the main themes of his work throughout his whole career to date?
Mechanics, Turbulence, Mach number, Boundary layer and Direct numerical simulation are his primary areas of study.
His study on Mechanics is mostly dedicated to connecting different topics, such as Classical mechanics.
Neil D. Sandham has researched Turbulence in several fields, including Flow, Compressibility and Trailing edge.
His Mach number research is multidisciplinary, incorporating perspectives in Acoustics, Compressible flow, Supersonic speed and Shock.
His research integrates issues of Oblique shock, Shock wave, Shock and Flow in his study of Boundary layer.
His Direct numerical simulation research focuses on subjects like Turbulence modeling, which are linked to K-epsilon turbulence model.
He most often published in these fields:
- Mechanics (77.54%)
- Turbulence (43.86%)
- Mach number (35.44%)
What were the highlights of his more recent work (between 2017-2021)?
- Mechanics (77.54%)
- Mach number (35.44%)
- Boundary layer (32.28%)
In recent papers he was focusing on the following fields of study:
His main research concerns Mechanics, Mach number, Boundary layer, Turbulence and Laminar flow.
His study in Mechanics concentrates on Reynolds number, Direct numerical simulation, Airfoil, Flow and Shock.
In his study, which falls under the umbrella issue of Direct numerical simulation, Compressible flow is strongly linked to Navier–Stokes equations.
His studies deal with areas such as Flow, Hypersonic speed, Instability, Freestream and Supersonic speed as well as Mach number.
His study in Boundary layer is interdisciplinary in nature, drawing from both Oblique shock, Shock wave, Surface finish, Work and Coolant.
Neil D. Sandham combines subjects such as Vorticity, Surface, Stall and Dissipative system with his study of Turbulence.
Between 2017 and 2021, his most popular works were:
- Direct numerical simulation of turbulent channel flow over a surrogate for Nikuradse-type roughness (26 citations)
- Shock-wave/boundary-layer interactions in the automatic source-code generation framework OpenSBLI (15 citations)
- Direct Numerical Simulations of Transonic Flow Around an Airfoil at Moderate Reynolds Numbers (10 citations)
In his most recent research, the most cited papers focused on:
- Quantum mechanics
- Mechanics
- Fluid dynamics
Neil D. Sandham mainly focuses on Mechanics, Mach number, Turbulence, Reynolds number and Direct numerical simulation.
Mechanics and Shock are commonly linked in his work.
Neil D. Sandham interconnects Acoustics, Hypersonic speed, Laminar flow, Pitot tube and Boundary layer in the investigation of issues within Mach number.
His studies in Turbulence integrate themes in fields like Plenum chamber, Streamlines, streaklines, and pathlines, Transition point and Vortex, Vorticity.
His Reynolds number research is multidisciplinary, relying on both Surface finish, Laminar-turbulent transition, Numerical stability, Airfoil and Mean flow.
His Direct numerical simulation research includes elements of Drag, Porosity, Smoothness and Scaling.
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