Nikolaos Perakis, M.Sc.

Wissenschaftlicher Mitarbeiter

Adresse:

Boltzmannstraße 15

85748 Garching b. München

Deutschland

Email:nikolaos.perakis@tum.de
Tel.:+49 (0) 89 289 -16176
Fax:+49 (0) 89 289 - 16166
Raum:MW 0629

Forschungsschwerpunkte

  • Modellierung und Simulation der Methan-Sauerstoff-Verbrennung
  • Simulation von Wärmetransportphänomenen in Raketenbrennkammern

Veröffentlichungen

Ausgewählte Veröffnetlichungen

  • Perakis, N., Strauß, J. and Haidn, O.J., 2019. “Heat flux evaluation in a multi-element CH4/O2 rocket combustor using an inverse heat transfer method”. International Journal of Heat and Mass Transfer, 142, p.118425, doi: 10.1016/j.ijheatmasstransfer.2019.07.075
  • Perakis, N., Rahn, D., Haidn, O.J. and Eiringhaus, D., 2019. “Heat Transfer and Combustion Simulation of Seven-Element O2/CH4 Rocket Combustor”. Journal of Propulsion and Power, pp.1-18, doi: 10.2514/1.B37402.
  • Hein, A.M., Perakis, N., Eubanks, T.M., Hibberd, A., Crowl, A., Hayward, K., Kennedy III, R.G. and Osborne, R., 2019. “Project Lyra: Sending a spacecraft to 1I/’Oumuamua (former A/2017 U1), the interstellar asteroid”. Acta Astronautica 161 (2019), doi: 10.1016/j.actaastro.2018.12.042.
  • Perakis, N., Haidn, O. J. “Inverse Heat Transfer Method applied to Capacitively Cooled Rocket Thrust Chambers“, International Journal of Heat and Mass Transfer 131 (2019): 150-166, doi: 10.1016/j.ijheatmasstransfer.2018.11.048
  • Breda, P., Pfitzner, M., Perakis, N. and Haidn, O., 2019. “Generation of non-adiabatic flamelet manifolds: comparison of two approaches applied on a single-element GCH4/GO2 combustion chamber”. In 8th European Conference for Aeronautics and Space Sciences (EUCASS).
  • Burkhardt, Z., Perakis, N., Welch, C., “Project Glowworm: Testing Laser Sail Propulsion in LEO”, 69th International Astronautical Congress 2018
  • Perakis, N., Rahn, D., Eiringhaus, D., Haidn, O. J. “Heat transfer and combustion simulation of a 7-element GOX/GCH4 rocket combustor”, 54th AIAA/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, 2018, doi: 10.2514/6.2018-4554
  • Perakis, N., Haidn, O. J., Rahn, D., Eiringhaus, D., Zhang, S., Daimon, Y., Karl, S., Horchler, T. “Qualitative and quantitative comparison of RANS simulation results for a 7 element GOX/GCH4 rocket combustor”, 54th AIAA/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, 2018, doi: 10.2514/6.2018-4556
  • Winter, F., Perakis, N., Haidn, O. J. “Emission Imaging of a GOX-GCH4 Coaxial Single Element Rocket Combustion Chamber”, 54th AIAA/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, 2018, doi: 10.2514/6.2018-4764
  • Perakis, N., Roth, C., Haidn, O. J. “Development of a non-adiabatic Flamelet model for reacting flows with heat loss”, Space Propulsion Conference 2018, Sevilla, Spain
  • Perakis, N., Roth, C., Haidn, O. J. “Simulation of a single-element rocket combustor using a non-adiabatic Flamelet model”, Space Propulsion Conference 2018, Sevilla, Spain