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TU Berlin

Inhalt des Dokuments

M.Sc. Leonie Malzacher

Wissenschaftliche Mitarbeiterin - Forschung & Lehre

Raum: F 013

Tel. +49 (0)30 314-29481
Fax +49 (0)30 314-79448



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


Publikationen

  • Aeroelastic Control of Compressor Blades in Transonic Flow Using Plasma Actuators
    V. Bicalho Civinelli de Almeida, V. Motta, L. Malzacher, T. D. Phan, R. Liebich,
    D. Peitsch
    ISUAAAT 15
    Oxford, UK,  September 24-27 2018, ISUAAAT15-069
  • 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
  • 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
  • Numerical investigation of virtual control surfaces for aeroelastic control on compressor blades
    V. Motta, L. Malzacher, D. Peitsch
    Journal of Fluids and Structures
    Volume 81, August 2018, Pages 617–637
    https://doi.org/10.1016/j.jfluidstructs.2018.06.002
  • Experimental Investigation of an Aerodynamic Mistuned Oscillating Compressor Cascade
    L. Malzacher, V. Motta, C. Schwarze, D. Peitsch
    ASME Turbo Expo 2018
    Oslo, Norway, June 11-15 2018, GT2018-75025
  • Aeroelastic Control on Compressor Blades with Virtual Control Surfaces: A Numerical Assessment
    V. Motta, L. Malzacher, V. Bicalho Civinelli de Almeida, D. Peitsch
    ASME Turbo Expo 2018
    Oslo, Norway, June 11-15 2018, GT2018-75079
  • A Physically Consistent Reduced Order Model for Plasma Aeroelastic Control on Compressor Blades
    V. Motta, L. Malzacher, D. Peitsch, G. Quaranta
    ASME Turbo Expo 2018
    Oslo, Norway, June 11-15 2018, GT2018-75080
  • Numerical Assessment of Virtual Control Surfaces for Load Alleviation on Compressor Blades
    V. Motta, L. Malzacher, D. Peitsch
    MDPI Applied Sciences,
    Volume 8, Issue 1, January 2018, 125
    www.mdpi.com/2076-3417/8/1/125
  • Numerical Investigation of Virtual Control Surfaces for Vibration Control on Compressor Blades
    V. Motta, L. Malzacher, D. Peitsch
    IFASD-2017 International Forum on Aeroelasticity and Structural Dynamics,
    Como, Italy, June 25-28 2017, IFASD-2017-137
  • 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
  • A low Speed Compressor Test Rig for Flutter Investigations
    L. Malzacher, S. Geist, D. Peitsch, H. Hennings
    ASME Turbo Expo 2016,
    Seoul, South Korea, June 13-17 2016, GT2016-57960
  • Experimental investigation of a turbine sealing cavity exposed to free stream pressure fluctuation
    T. Schliwka, L. Malzacher, S. Chemnitz, D. Peitsch
    Active Flow and Combustion Control 2014,
    Berlin, Germany, September 10-12 2014
  • Simulation and validation of low pressure turbine transition parameters
    L. Malzacher, C. Lyko, D. Peitsch
    15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC-15
    Honolulu, Hawaii, USA, February 24-28 2014, ISROMAC-TU308
  • Die Entwicklung einer Mess-Strecke mit optischem Zugang für den Heiß-Akustik-Teststand in Berlin
    T. Schliwka, L. Malzacher, D. Peitsch
    Deutscher Luft- und Raumfahrtkongress 2013,
    Stuttgart, Germany, September 10-12 2013, DLRK-2013-301366

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