Ralf Deiterding

ORCID: 0000-0003-4776-8183
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About
Contact & Profiles
Research Areas
  • Combustion and Detonation Processes
  • Computational Fluid Dynamics and Aerodynamics
  • Fire dynamics and safety research
  • Gas Dynamics and Kinetic Theory
  • Lattice Boltzmann Simulation Studies
  • Fluid Dynamics and Turbulent Flows
  • Fluid Dynamics and Vibration Analysis
  • Aerodynamics and Fluid Dynamics Research
  • Energetic Materials and Combustion
  • Plasma and Flow Control in Aerodynamics
  • Combustion and flame dynamics
  • Aerosol Filtration and Electrostatic Precipitation
  • Aerodynamics and Acoustics in Jet Flows
  • Advanced Numerical Methods in Computational Mathematics
  • Wind and Air Flow Studies
  • Fluid Dynamics Simulations and Interactions
  • Risk and Safety Analysis
  • Advanced Fiber Laser Technologies
  • Structural Response to Dynamic Loads
  • Particle Dynamics in Fluid Flows
  • Photonic Crystal and Fiber Optics
  • Astro and Planetary Science
  • Laser-Plasma Interactions and Diagnostics
  • Vehicle emissions and performance
  • Planetary Science and Exploration

University of Southampton
2015-2024

Tianjin University
2022

National University of Defense Technology
2017-2021

Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
2013-2016

Oak Ridge National Laboratory
2007-2015

University of Tennessee at Knoxville
2011

California Institute of Technology
2005-2007

Obtaining a rapid deflagration-to-detonation transition (DDT) within short smooth tube is challenging task. Here, an unconventional means of flame acceleration propagating upstream in subsonic and supersonic mixtures was introduced to acquire speedy DDT. The Navier–Stokes equations with adaptive mesh refinement technique detailed hydrogen–air chemistry reaction mechanism 11 species 27 steps were utilized resolve the entire DDT characteristics. effect initial Mach number on revealed...

10.1063/5.0191500 article EN Physics of Fluids 2024-03-01

Structured adaptive mesh refinement (SAMR) techniques can enable cutting-edge simulations of problems governed by conservation laws. Focusing on the strictly hyperbolic case, these notes explain all algorithmic and mathematical details a technically relevant implementation tailored for distributed memory computers. An overview background commonly used finite volume discretizations gas dynamics is included typical benchmarks to quantify accuracy performance dynamically code are discussed....

10.1051/proc/201134002 article EN ESAIM Proceedings 2011-12-01

Numerical simulation can be key to the understanding of multidimensional nature transient detonation waves. However, accurate approximation realistic detonations is demanding as a wide range scales needs resolved. This paper describes successful solution strategy that utilizes logically rectangular dynamically adaptive meshes. The hydrodynamic transport scheme and treatment nonequilibrium reaction terms are sketched. A ghost fluid approach integrated into method allow for embedded...

10.1155/2011/738969 article EN cc-by Journal of Combustion 2011-01-01

In detonation engines and accidental explosions, a may propagate in an inhomogeneous mixture with non-uniform reactant concentration. this study, one- two-dimensional simulations are conducted for propagation hydrogen/oxygen/nitrogen mixtures periodic sinusoidal or square wave distribution of the The objective is to assess properties such mixtures. Specifically, quenching reinitiation, cellular structure, cell size speed deficit investigated. It found that there exists critical amplitude...

10.1017/jfm.2022.1074 article EN Journal of Fluid Mechanics 2023-01-16

A virtual test facility (VTF) for studying the three-dimensional dynamic response of solid materials subject to strong shock and detonation waves has been constructed as part research program Center Simulating Dynamic Response Materials at California Institute Technology. The compressible fluid flow is simulated with a Cartesian finite volume method treating an embedded moving body, while Lagrangian element scheme employed describe structural hydrodynamic pressure loading. temporal splitting...

10.1007/s00366-006-0043-9 article EN cc-by-nc Engineering With Computers 2006-10-18

10.1016/j.proci.2006.07.244 article EN Proceedings of the Combustion Institute 2006-09-26

Abstract An experimental and computational investigation of the unsteady separation behaviour two spheres in Mach-4 flow is carried out. The spherical bodies, initially contiguous, are released with negligible relative velocity thereafter fly freely according to aerodynamic forces experienced. In experiments performed a supersonic Ludwieg tube, nylon suspended test section by weak threads which detached arrival flow. subsequent sphere motions structures recorded using high-speed (13 kHz)...

10.1017/jfm.2012.453 article EN Journal of Fluid Mechanics 2012-10-26

The extension to the split-step Fourier method (SSFM) for Schrödinger-type pulse propagation equations that we propose in this article is designed with accurate simulation of pulses femto-second regime single-mode communication fibers mind. We show via an appropriate operator splitting scheme, Kerr nonlinearity and self-steepening stimulated Raman scattering terms can be combined into a single sub-step consisting inhomogeneous quasilinear first-order hyperbolic system real-valued quantities...

10.1109/jlt.2013.2262654 article EN Journal of Lightwave Technology 2013-05-21

A large-eddy simulation is conducted to investigate the transient structure of an unstable detonation wave in two dimensions and evolution intrinsic hydrodynamic instabilities. The dependency on grid resolution investigated, structures obtained by are compared with predictions from solving Euler Navier–Stokes equations directly. results indicate that predict irregular agreement experimental observations vorticity generation dissipation small scale should be taken into account. Thus, high...

10.2514/1.b34986 article EN Journal of Propulsion and Power 2014-01-31

The main objective of this work is to comprehensively provide a fundamental understanding the entire process flame-pressure wave interactions with end-gas autoignition and detonation development in confined chamber by two-dimensional numerical simulations stoichiometric hydrogen/air mixture. flame dynamics, pressure propagation, its structure evolution, together mechanism end gas, are analyzed detail. Six stages, including spherical flame, finger skirt touching sidewalls, interactions,...

10.1063/1.5099456 article EN Physics of Fluids 2019-07-01

Hypersonic flows involving two or more bodies travelling in close proximity to one another are encountered several important situations. The present work seeks explore aspect of the resulting flow problem by investigating forces experienced a secondary body when it is within domain influence primary at hypersonic speeds. An analytical methodology based on blast wave analogy developed and used predict force coefficients for simple geometries both three dimensions. When entirely inside shocked...

10.1017/s0022112007007987 article EN Journal of Fluid Mechanics 2007-10-15
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