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Thomas Behrendt

Researcher at German Aerospace Center

Publications -  33
Citations -  321

Thomas Behrendt is an academic researcher from German Aerospace Center. The author has contributed to research in topics: Combustor & Combustion chamber. The author has an hindex of 10, co-authored 33 publications receiving 276 citations.

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Journal ArticleDOI

PLIF Thermometry Based on Measurements of Absolute Concentrations of the OH Radical

TL;DR: In this paper, a method for measurements of planar temperature distributions based on planar laser-induced fluorescence (PLIF) of the OH radiacal is described, which was developed specifically for the application in lean combustion systems, where OH equilibrium concentrations are largely independent on equivalence ratio and a function of temperature only.
Journal ArticleDOI

Experimental and Numerical Investigation of a Planar Combustor Sector at Realistic Operating Conditions

TL;DR: In this paper, the results of an ongoing collaboration between the engine manufacturer MTU and the German aerospace research center DLR on the NO x reduction potential of conventional combustors are reported.
Proceedings ArticleDOI

Characterization of Advanced Combustor Cooling Concepts Under Realistic Operating Conditions

TL;DR: In this paper, the effect of cooling air properties on the cooling effectiveness of different advanced cooling concepts at realistic operating conditions is presented and analyzed and an introduction into basic cooling design considerations is included in the article.
Proceedings ArticleDOI

Improvement of Oxide/Oxide CMC and Development of Combustor and Turbine Components in the HiPOC Program

TL;DR: In this paper, three different oxide/oxide ceramic matrix composite (CMC) materials are described and the design concepts for the attachment of the CMC component to the metal structure of the gas turbine are developed in a first work stream focused on the combustion chamber and the turbine seal segment.
Journal ArticleDOI

A test rig for investigations of gas turbine combustor cooling concepts under realistic operating conditions

TL;DR: In this paper, a new test rig for the characterization of advanced combustor cooling concepts for gas turbine combustors is presented, which is designed to allow investigations at elevated pressures and temperatures representing realistic operating conditions of future lean low emission combustors.