Wolfgang Schröder

ORCID: 0000-0002-3472-1813
Publications
Citations
Views
---
Saved
---
About
Contact & Profiles
Research Areas
  • Fluid Dynamics and Turbulent Flows
  • Aerodynamics and Acoustics in Jet Flows
  • Computational Fluid Dynamics and Aerodynamics
  • Combustion and flame dynamics
  • Wind and Air Flow Studies
  • Fluid Dynamics and Vibration Analysis
  • Particle Dynamics in Fluid Flows
  • Aerodynamics and Fluid Dynamics Research
  • Heat Transfer Mechanisms
  • Lattice Boltzmann Simulation Studies
  • Solar and Space Plasma Dynamics
  • Advanced Combustion Engine Technologies
  • Physics and Engineering Research Articles
  • Ionosphere and magnetosphere dynamics
  • Turbomachinery Performance and Optimization
  • Gas Dynamics and Kinetic Theory
  • Plasma and Flow Control in Aerodynamics
  • Acoustic Wave Phenomena Research
  • Geophysics and Gravity Measurements
  • Geomagnetism and Paleomagnetism Studies
  • Environmental Science and Technology
  • History and Developments in Astronomy
  • Aerosol Filtration and Electrostatic Precipitation
  • Fluid Dynamics and Heat Transfer
  • Atmospheric Ozone and Climate

RWTH Aachen University
2016-2025

University of Cologne
1997-2025

University Hospital Cologne
2013-2025

Forschungszentrum Jülich
2015-2024

Jülich Aachen Research Alliance
2016-2024

Centrum für Integrierte Onkologie
2024

China Aerodynamics Research and Development Center
2009-2024

Massachusetts General Hospital
2023

FH Aachen
2001-2020

Leibniz Institute for Tropospheric Research
2004-2019

A possible strategy for the reduction of aeroacoustic noise generated by turbulence interacting with a wing profile, also referred to as leading-edge noise, is represented implementation porous medium in structure airfoil. However, physical mechanisms involved this mitigation technique remain unclear. The present work aims at elucidating these phenomena and particularly how porosity affects incoming characteristics immediate vicinity surface. NACA-0024 profile equipped melamine foam has been...

10.1016/j.jsv.2020.115561 article EN cc-by-nc-nd Journal of Sound and Vibration 2020-07-05

Large-eddy simulations are performed to investigate turbulent flows through 90° pipe bends that feature unsteady flow separation, unstable shear layers, and an oscillation of the Dean vortices. Single with curvature radii one- three-pipe diameters considered at Reynolds number range 5000–27 000. The numerically computed distributions time-averaged velocities, stress components, power spectra velocities validated by comparison particle image velocimetry measurements. overall forces onto walls...

10.1063/1.1852573 article EN Physics of Fluids 2005-02-08

Owls are known for their silent flight. Even though there is some information available on the mechanisms that lead to a reduction of noise emission, neither morphological basis, nor biological owl's flight known. Therefore, we have initiated systematic analysis wing morphology in both specialist, barn owl, and generalist, pigeon. This report presents comparison between feathers owl pigeon emphasise specific characteristics macroscopic microscopic level. An understanding features underlying...

10.1186/1742-9994-4-23 article EN cc-by Frontiers in Zoology 2007-01-01

10.1016/j.compfluid.2005.02.007 article EN Computers & Fluids 2005-08-27

10.1016/j.ijheatfluidflow.2007.07.010 article EN International Journal of Heat and Fluid Flow 2007-12-04

To support Lee's buffet mechanism model [B. H. K. Lee, “Self-sustained shock oscillations on airfoils at transonic speeds,” Prog. Aerosp. Sci. 37, 147–196 (2001)10.1016/S0376-0421(01)00003-3], the sound wave propagation in flow field outside separation of a Mach number M∞ = 0.73 and an angle attack α 3.5° over DRA 2303 supercritical airfoil is determined using high-speed particle-image velocimetry. Furthermore, influenced by artificial source which evidently changes oscillation properties....

10.1063/1.4791603 article EN Physics of Fluids 2013-02-01

Although low-disturbance ("quiet") hypersonic wind tunnels are believed to provide more reliable extrapolation of boundary-layer transition behavior from ground flight, the presently available quiet facilities limited Mach 6, moderate Reynolds numbers, low freestream enthalpy, and subscale models. As a result, only conventional ("noisy") can reproduce both numbers enthalpies flight configurations must therefore be used for vehicle test evaluation involving high number, larger This paper...

10.2514/1.a34290 article EN publisher-specific-oa Journal of Spacecraft and Rockets 2018-11-30

The Air Quality Model Evaluation International Initiative (AQMEII) has now reached its second phase which is dedicated to the evaluation of online coupled chemistry-meteorology models. Sixteen modeling groups from Europe and five North America have run regional air quality models simulate year 2010 over one European American domain. MACC re-analysis been used as chemical initial (IC) boundary conditions (BC) by all participating in AQMEII-2. aim present work evaluate along with against a set...

10.1016/j.atmosenv.2015.02.034 article EN cc-by-nc-nd Atmospheric Environment 2015-02-11
Coming Soon ...