Felix Hötte, M. Sc.

Publications

Journals (peer-reviewed):

• Hötte, F.; Haupt, M.C.: Transient 3D Conjugate Heat Transfer Simulation of a Rectangular GOX-GCH4 Rocket Combustion Chamber and Validation, Aerospace Science and Technology, Vol. 105, Elsevier, 2020, doi: https://doi.org/10.1016/j.ast.2020.106043
• Hötte, F.; von Sethe, C.; Fiedler, T.; Haupt, M.C.; Haidn, O.J.; Rohdenburg, M.: Experimental Lifetime Study of Regeneratively Cooled Rocket Chamber Walls, International Journal of Fatigue, Vol. 138, Elsevier, 2020, doi: https://doi.org/10.1016/j.ijfatigue.2020.105649
• Hötte, F.; Lungu, P.; von Sethe, C.; Fiedler, T.; Haupt, M.C.; Haidn, O.J.: Experimental Investigations of Thermomechanical Fluid-Structure Interaction in Rocket Combustion Chambers, Journal of Propulsion and Power, Vol. 35(5), Pages 906-916, AIAA, 2019, doi: https://doi.org/10.2514/1.B37439
• Haupt, M.C.; Kowollik, D.; Lindhorst, K.; Hötte, F.: Fluid-Structure-Interaction in Rocket Thrust Chambers Simulation and Validation. Defect and Diffusion Forum, Vol. 366, Pages 97-117, Trans Tech Publications Ltd, 2016, doi:  https://doi.org/10.4028/www.scientific.net/DDF.366.97

Books:

• Hötte, F.; Günther, O.; v. Sethe, C.; Haupt, M.; Scholz, P.: Lifetime Experiments of Regeneratively Cooled Rocket Combustion Chambers and PIV Measurements in a High Aspect Ratio Cooling Duct. In: Adams, N. et al. (eds): Future Space-Transport-System Components under High Thermal and Mechanical Loads. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 146. Springer, Cham, 2021, doi: https://doi.org/10.1007/978-3-030-53847-7_18
• Barfusz, O.; Hötte, F.; Reese, S.; Haupt, M.: Pseudo-transient 3D Conjugate Heat Transfer Simulation and Lifetime Prediction of a Rocket Combustion Chamber. In: Adams, N. et al. (eds): Future Space-Transport-System Components under High Thermal and Mechanical Loads. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 146. Springer, Cham, 2021, doi: https://doi.org/10.1007/978-3-030-53847-7_17
• Fiedler, T.; Rösler, J.; Bäker, M.; Hötte, F.; v. Sethe, C.; Daub, D.; Haupt, M.; Haidn, O.; Esser, B.; Gülhan, A.: Mechanical Integrity of Thermal Barrier Coatings - Coating Development and Micromechanics. In: Adams, N. et al. (eds): Future Space-Transport-System Components under High Thermal and Mechanical Loads. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 146. Springer, Cham, 2021, doi: https://doi.org/10.1007/978-3-030-53847-7_19

Conferences:

• Hötte, F.; Lungu, P.; Haupt, M.C.; Haidn, O.J.: Experimental and numerical investigations of thermo-mechanical fluid-structure interaction in cooled rocket combustion chambers. 54th AIAA/SAE/ASEE Joint Propulsion Conference, Cincinnati, Ohio, July 9-11, 2018, doi: https://doi.org/10.2514/6.2018-4767
• Martin, K.; Daub, D.; Hötte, F.; Reese, S.; Esser, B.; Gülhan, A.; Haupt, M.C.: Simulationsmethoden und experimentelle Validierung für thermisches Beulen dünnwandiger Strukturen unter aerothermodynamischen Lasten. 66. Deutscher Luft- und Raumfahrtkongress (DLRK), München, 2017

Annual Reports:

• Barfusz, O.; Hötte, F.; Reese, S.; Haupt, M.C.: Lifetime analysis of a virtual thrust chamber demonstrator and 11-domain conjugate heat transfer simulation of a rocket combustion chamber. SFB TRR 40,  Technische Universität München - Lehrstuhl für Aerodynamik und Strömungsmechanik, Annual Report, 2019. https://www.researchgate.net/publication/339570310_Lifetime_analysis_of_a_virtual_thrust_chamber_demonstrator_and_11-domain_conjugate_heat_transfer_simulation_of_a_rocket_combustion_chamber
• Hötte, F.; Günther, O.; Rohdenburg, M.; Haupt, M.C.; Scholz, P.: Roughness and Crack Investigations of Rocket Combustion Chambers and Pressure Loss Measurements in a High Aspect Ratio Cooling Duct. SFB TRR 40,  Technische Universität München - Lehrstuhl für Aerodynamik und Strömungsmechanik, Annual Report, 2019. https://www.researchgate.net/publication/339570304_Roughness_and_Crack_Investigations_of_Rocket_Combustion_Chambers
  _and_Pressure_Loss_Measurements_in_a_High_Aspect_Ratio_Cooling_Duct
• Barfusz, O.; Hötte, F.; Reese, S.; Haupt, M.C.: Constitutive modeling with finite element technology for anisotropic nozzle extensions along with conjugate heat transfer in a rocket combustion chamber. SFB TRR 40,  Technische Universität München - Lehrstuhl für Aerodynamik und Strömungsmechanik, Annual Report, 2018
• Hötte, F.; Günther, O.; Lungu, P.; Haupt, M.C.; Scholz, P.; Haidn, O.J.: Life time experiments of rocket combustion chamber structures and cooling channel flow characterization. SFB TRR 40,  Technische Universität München - Lehrstuhl für Aerodynamik und Strömungsmechanik, Annual Report, 2017
• Barfusz, O.; Hötte, F.; Reese, S.; Haupt, M.C.: Numerical modelling of CMC nozzle structures and cooling channel flow simulation. SFB TRR 40,  Technische Universität München - Lehrstuhl für Aerodynamik und Strömungsmechanik, Annual Report, 2017
• Hötte, F.; Celano, M.P.; Rochlitz, H.; Haupt, M.C.; Haidn, O.J.; Scholz, P.: Experimental investigations for cooling channel structure lifetime, rocket combustion chamber and cooling channel flow characterization. SFB TRR 40,  Technische Universität München - Lehrstuhl für Aerodynamik und Strömungsmechanik, Annual Report, 2016
• Fassin, M.; Hötte, F.; Reese, S.; Haupt, M.C.: Lifetime influence of thermal barrier coatings and thermal analysis of the fatigue experiment. SFB TRR 40,  Technische Universität München - Lehrstuhl für Aerodynamik und Strömungsmechanik, Annual Report, 2016
• Celano, M. P.; Rochlitz, H.; Hötte, F.; Haidn, O. J.; Scholz, P. & Haupt, M. C.: Experimental investigation on heat transfer of rocket combustion chambers and cooling channels. SFB TRR 40,  Technische Universität München - Lehrstuhl für Aerodynamik und Strömungsmechanik, Annual Report, 2015