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Tim Horchler
Tim Horchler
Bestätigte E-Mail-Adresse bei dlr.de
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Zitiert von
Zitiert von
Jahr
Qualitative and quantitative comparison of RANS simulation results for a 7-element GOX/GCH4 rocket combustor
N Perakis, OJ Haidn, D Eiringhaus, D Rahn, S Zhang, Y Daimon, S Karl, ...
2018 Joint Propulsion Conference, 4556, 2018
452018
Hybrid RANS-LES study of transonic flow in the wake of a generic space launch vehicle
T Horchler, K Oßwald, V Hannemann, K Hannemann
Progress in Hybrid RANS-LES Modelling: Papers Contributed to the 6th …, 2018
82018
Modeling combustion chamber acoustics using the DLR TAU code
T Horchler, W Armbruster, J Hardi, S Karl, K Hannemann, A Gernoth, ...
Space Propulsion Conference, 2018
62018
Dynamic mode decomposition of backward facing step flow simulation data
T Horchler, KV Mani, K Hannemann
22nd AIAA Computational Fluid Dynamics Conference, 3411, 2015
52015
Efficient handling of cryogenic equation of state for the simulation of rocket combustion chambers
S Fechter, T Horchler, S Karl, K Hannemann, D Suslov, J Hardi, ...
Non-Ideal Compressible Fluid Dynamics for Propulsion and Power: Selected …, 2020
42020
A timescale-augmented spalart-allmaras turbulence model for flamelet combustion applications
T Horchler, S Fechter, S Karl, K Hannemann
Proceedings of the 8th European Conference for Aeronauticas and Aerospace …, 2019
42019
Numerical investigation of flame-acoustic interaction at resonant and non-resonant conditions in a model combustion chamber
T Horchler, S Fechter, J Hardi
Aerospace 11 (7), 1-24, 2024
32024
Skalenauflösende Simulation der Flammen-Akustik-Wechselwirkung bei resonanter und nicht-resonanter Anregung in einer Experimental-Raketenbrennkammer
T Horchler
Justus-Liebig-Universität Gießen, 2022
32022
Rest hf-10 test case: Numerical simulation of a single coaxial lox-ch4 injector with forced mass flow oscillations using the dlr tau-code
T Horchler, S Fechter, J van Schyndel, M Oschwald
9th European Conference for Aeronautics and Aerospace Sciences (EUCASS), 1-14, 2022
32022
Rest hf-10 test case: Synthesis of the contributions for the simulation of excited methane flames under real gas conditions
S Thomas, R Kaess, R Behr, S Koeglmeier, O Knab, T Horchler, ...
9TH European Conference for Aeronautics and Aerospace Sciences, 2022
32022
Influence of numerical model setup on the response of acoustically forced LOx/H2 flames
F Tonti, J Hardi, T Horchler, S Fechter, M Oschwald
Proceedings of the 8th European Conference for Aeronautics and Space Sciences, 2019
32019
Selection Rules for Resonant Longitudinal Injector-Coupling in Experimental Rocket Combustors
T Horchler
Aerospace 9 (11), 669, 2022
22022
Comparison of detailed chemistry and flamelet combustion modeling in a H2/LOx subscale combustion chamber
T Horchler, S Fechter, S Karl, K Hannemann
17th International Conference on Numerical Combustion 2019, 2019
22019
Investigation of rans turbulence models for cryogenic rocket combustion chambers
S Fechter, T Horchler, S Karl, K Hannemann
8th European Conference for Aeronautics and Space Sciences (EUCASS), 2019
22019
Numerical and experimental investigation of the shockwave boundary layer interaction of laminar/transitional flow past a sharp fin
T Ecker, J Martinez Schramm, L Schmidt, D Surujhlal, A Wagner, ...
10th EUCASS–9th CEAS 2023, 2023
12023
Development of a photon Monte Carlo radiative heat transfer solver for CFD applications
G Oblapenko, T Ecker, S Fechter, T Horchler, S Karl
Joint 10th EUCASS—9th CEAS Conference, 2023
12023
Generic numerical test case to understand cryogenic methane combustion dynamics
S Fechter, T Horchler, S Karl, K Hannemann
Proceedings of the 3rd International Seminar on Non-Ideal Compressible Fluid …, 2021
12021
Numerical simulation of cryogenic flows under high-pressure conditions
S Fechter, T Horchler, S Karl, K Hannemann
17th International Conference on Numerical Combustion 2019, 2019
12019
DLR Project TAUROS: TAU for Rocket Thrust Chamber Simulation
D Schneider, J Hardi, J Martin, R Stark, D Suslov, F Tonti, J Van Schyndel, ...
Proceedings of the 8th European Conference for Aeronautics and Space Sciences, 2019
12019
Application of HyperCODA to Hypersonic Flows Around Two-Dimensional Geometries
C Amato, T Ecker, T Horchler, S Fechter, I Huismann
3rd International Conference on High-Speed Vehicle Science and Technology …, 2024
2024
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