Phase-locked two-line OH planar laser-induced fluorescence thermometry in a pulsating gas turbine model combustor at atmospheric pressure
Manfred Aigner's research works | German Aerospace Center (DLR), Köln (DLR) and other places
Manfred Aigner's research works | German Aerospace Center (DLR), Köln (DLR) and other places
Oxidation-Induced Damage Modeling in Micro Gas-Turbines Combustion Chambers - YouTube
Feedstocks a major hurdle for sustainable aviation fuels adoption - F&L Asia
Manfred Aigner's research works | German Aerospace Center (DLR), Köln (DLR) and other places
DLR - Institute of Combustion Technology - Home
Toward finite-rate chemistry large-eddy simulations of sooting swirl flames: Combustion Science and Technology: Vol 190, No 7
Manfred Aigner's research works | German Aerospace Center (DLR), Köln (DLR) and other places
aireg General Assembly elects Manfred Aigner as President for Science and Research - Aviation Initiative for Renewable Energy in Germany e.V.
Modelling of combustion acoustics sources and their dynamics in the PRECCINSTA burner test case - Felix Grimm, Jürgen Dierke, Roland Ewert, Berthold Noll, Manfred Aigner, 2017
Energies | Free Full-Text | Numerical and Experimental Study of a Jet-and-Recirculation Stabilized Low Calorific Combustor for a Hybrid Power Plant
Manfred Aigner's research works | German Aerospace Center (DLR), Köln (DLR) and other places
Prediction of Combustion Noise for an Aeroengine Combustor | Journal of Propulsion and Power
Fuels of the future put to the test | en:former
![PDF] Experimental analysis of the combustion behaviour of oxyfuel flames in a gas turbine model combustor | Semantic Scholar](https://d3i71xaburhd42.cloudfront.net/2ef58acee92580a52e5899d566e1076fec0a2c63/21-Figure1-1.png "PDF] Experimental analysis of the combustion behaviour of oxyfuel flames in a gas turbine model combustor | Semantic Scholar")
PDF] Experimental analysis of the combustion behaviour of oxyfuel flames in a gas turbine model combustor | Semantic Scholar
Assumed PDF Modeling in Rocket Combustion Simulations
Phase-locked two-line OH planar laser-induced fluorescence thermometry in a pulsating gas turbine model combustor at atmospheric pressure
Accelerate Hydrogen Adoption Using Simulation
![PDF] Experimental analysis of the combustion behaviour of oxyfuel flames in a gas turbine model combustor | Semantic Scholar](https://d3i71xaburhd42.cloudfront.net/2ef58acee92580a52e5899d566e1076fec0a2c63/22-Figure2-1.png "PDF] Experimental analysis of the combustion behaviour of oxyfuel flames in a gas turbine model combustor | Semantic Scholar")
PDF] Experimental analysis of the combustion behaviour of oxyfuel flames in a gas turbine model combustor | Semantic Scholar
DLR Events | 11:00 – 11:30 CEST | Sustainable aviation fuels: perspective for aviation and example for technology transfer
