Luftfahrtantriebe

M.Sc. Nicolai Neumann

M.Sc.

Nicolai Neumann

Wissenschaftlicher Mitarbeiter

nicolai.neumann@tu-berlin.de

+49 30 314-29055

+49 30 314-79448

Einrichtung Fachgebiet Luftfahrtantriebe
Sekretariat F1
Gebäude F
Raum F 016
Sprechstundetbd

Postanschrift

Technische Universität Berlin
Institut für Luft- und Raumfahrt
Fachgebiet Luftfahrtantriebe
Sekretariat F1
Marchstraße 12-14
D-10587 Berlin

Publikationen

2022

Neumann, N.; Rähse, T.; Stathopoulos, P.; Peitsch, D.
Numerical Analysis of Unsteady Compressor Performance Under Boundary Conditions Caused by Pulsed Detonation Combustion
In King, Rudibert and Peitsch, Dieter, Editor, Active Flow and Combustion Control 2021Band152ausNotes on Numerical Fluid Mechanics and Multidisciplinary Design, Seite 272–287
In King, Rudibert and Peitsch, Dieter, Editor
Herausgeber: Springer International Publishing, Cham
2022
ISBN
978-3-030-90727-3

2021

Asli, M.; Garan, N.; Neumann, N.; Stathopoulos, P.
A Robust One-Dimensional Approach for the Performance Evaluation of Turbines Driven by Pulsed Detonation Combustion
Energy Conversion and Management, 248 :114784
November 2021
Herausgeber: Elsevier Ltd.
ISSN: 0196-8904
Neumann, N.; Asli, M.; Garan, N.; Peitsch, D.; Stathopoulos, P.
A Fast Approach for Unsteady Compressor Performance Simulation Under Boundary Condition Caused by Pressure Gain Combustion
Applied Thermal Engineering, 196 :117223
September 2021
Herausgeber: Elsevier Ltd.
ISSN: 1359-4311
Neumann, N.; Berthold, A.; Haucke, F.; Peitsch, D.; Stathopoulos, P.
Pulsed Impingement Turbine Cooling and its Effect on the Efficiency of Gas Turbines with Pressure Gain Combustion
Band 143
Herausgeber: ASME
April 2021

2019

Neumann, N.; Woelki, D.; Peitsch, D.
A Comparison of Steady-State Models for Pressure Gain Combustion in Gas Turbine Performance Simulation
In GPPS, Editor
September 2019
Neumann, N.; Peitsch, D.
Introduction and Validation of a Mean Line Solver for Present and Future Turbomachines
In ISABE, Editor
September 2019
Neumann, N.; Peitsch, D.
Potentials for Pressure Gain Combustion in Advanced Gas Turbine Cycles
Journal of Applied Sciences, 9 (16) :3211
August 2019
Creative Commons Attribution 4.0 International License CC-BY 4.0
Herausgeber: MDPI
ISSN: 2076-3417