Uwe Koch
German Aerospace Center
Network
Latest external collaboration on country level. Dive into details by clicking on the dots.
Publication
Featured researches published by Uwe Koch.
Journal of Spacecraft and Rockets | 2009
Ali Gülhan; Burkard Esser; Uwe Koch; Frank Siebe; Johannes Riehmer; Domenico Giordano; Detlev Konigorski
This paper describes an experimental study on heat-flux mitigation within high-enthalpy ionized-argon flows by application of an external magnetic-induction field. Two different axially symmetric test models containing water-cooled magnet coils have been investigated. The models have been made of a material with low thermal conductivity to visualize surface-temperature distribution.The latter has been measured by infrared thermography. Heat-flux rates have been derived from measured front- and rear-surface temperatures, taking into account temperature-dependent material characteristics and considering radiative-cooling exchange to the environment. Flowfield properties have been quantitatively characterized by laser-induced fluorescence, microwave interferometry, emission spectroscopy, electrostatic probes, and pitot probes. In addition, high-quality video recordings and photographs have been taken for shock-layer visualization. Remarkable measured surface-temperature reductions (16 and 44%) and derived heat-flux mitigations (46 and 85%) have been observed in the presence of an externally applied magnetic-induction field.
42nd AIAA Thermophysics Conference | 2011
Min Kwan Kim; Burkard Esser; Uwe Koch; Ali Guelhan
In the present study, we describe the end-to-end model of a plasma wind tunnel. A plasma wind tunnel is an useful facility for the ground-based experiment of high enthalpy flows including hypersonic flows, because it can provides a similar flow environment which is experienced by a vehicle during hypersonic flights. For the experimental research of high enthalpy flows, the German Aerospace Center (DLR) Cologne research facility has an arc heated plasma wind tunnel, L3K. The accurate prediction of flow characteristics is very important to calibrate measurement devices and choose measurement methods in a plasma wind tunnel experiment. However, it is difficult to understand the detailed flow conditions of a plasma wind tunnel, because the flow inside a plasma wind tunnel is usually in strong chemical and thermal non-equilibrium state. we numerically simulate a high enthalpy flow inside a plasma wind tunnel using a multi-temperature model and compare with the measured data using CARS method. The numerical model of a plasma wind tunnel will be useful to design a new wind tunnel and determine flow conditions at the test section of a plasma wind tunnel.
Journal of Thermophysics and Heat Transfer | 2018
Giuseppe. Ceglia; A. Del Vecchio; Uwe Koch; Burkard Esser; Ali Guelhan
An experimental investigation of high-enthalpy air flow generated by L2K arc-jet facility of DLR is carried out by means of two-photon absorption laser-induced fluorescence (TALIF) measurements of ...
AIAA Journal | 2017
Ali Gülhan; Burkard Esser; Uwe Koch; Michael Fischer; Eggert Magens; Volker Hannemann
For reliable material qualification in high-enthalpy flows, detailed characterization of material and flow parameters is essential. Therefore, the flowfield of arc-heated facility L3K, which has be...
Archive | 2004
Uwe Koch; Burkard Esser; Ali Gülhan
Journal of Spacecraft and Rockets | 2001
Ali Gülhan; Burkard Esser; Uwe Koch
Progress in Flight Physics | 2017
Lars Steffens; Uwe Koch; Burkard Esser; Ali Gülhan
Archive | 2015
Burkard Esser; Ali Gülhan; Uwe Koch
40th AIAA Plasmadynamics and Lasers Conference | 2009
Ali Gülhan; Burkard Esser; Uwe Koch; Frank Siebe; Johannes Riehmer; Domenico Giordano
Archive | 2008
Uwe Koch; Johannes Riehmer; Burkard Esser; Ali Gülhan