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

• Dynamic mode decomposition analysis of plasma aeroelastic control of airfoils in cascade
  P. Neumann, V. Bicalho Civinelli de Almeida, V. Motta, L. Malzacher,
  D. Peitsch, G. Quaranta
  Journal of Fluids and Structures,
  Volume 94, April 2020, 102901
  DOI: 10.1016/j.jfluidstructs.2020.102901
• Numerical Investigation of Flutter Stability on a Compressor Cascade with Variable Inflow Conditions
  P. Neumann, L. Malzacher, V. Motta, D. Peitsch
  ISUAAAT 15,
  Oxford, UK,  September 24-27 2018, ISUAAAT15-016
• A CFD Assessment of Virtual Surfaces for Aeroelastic Control on Compressor Blades with an Experimentally Tuned Plasma Actuator Model
  S. Cavallo, V. Motta, P. Neumann, L. Malzacher, M. G. De Giorgi, D. Peitsch
  ISUAAAT 15,
  Oxford, UK,  September 24-27 2018, ISUAAAT15-068
• Reduced Order Modeling for Plasma Aeroelastic Control of Airfoils in Cascade: Dynamic Mode Decomposition
  P. Neumann, V. Motta, L. Malzacher, D. Peitsch, G. Quaranta
  IUTAM 2018,
  Santorini, Greece, June 18-22 2018
• Numerical Assessment of Virtual Control Surfaces for Compressor Blades
  V. Motta, L. Malzacher, P. Neumann, D. Peitsch
  35th AIAA Applied Aerodynamics Conference,
  Denver, USA, June 5-9 2017, AIAA 2017-3909