direkt zum Inhalt springen

direkt zum Hauptnavigationsmenü

Sie sind hier

TU Berlin

Inhalt des Dokuments

Publikationen am FG Aerodynamik

<< zurück [1]
vor >> [15]

P

Active flow control by means of synthetic jets on a highly loaded compressor cascade [19]

Zander, V., Hecklau, M., Nitsche, W., Huppertz, A. and Swoboda, M.

Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 897-906. 2011

Download Bibtex Eintrag [20]

Active Control of the Corner Separation on a Highly Loaded Compressor Cascade with Periodic Non-Steady Boundary Conditions by means of Fluidic Actuators [21]

Staats, M. and Nitsche, W.

Proceedings of the ASME Turbo Expo 2015, June 15-18, Montreal, Canada, ASME paper GT2015-42161 2015

Download Bibtex Eintrag [22]

Numerical Simulation of a Large Pressure-Induced Turbulent Separation Bubble [23]

Mohammed-Taifour, A., Dufresne, L. and Weiss, J.

Proceedings of the 27th CANCAM, Sherbrooke, QC, Canada 2019

Download Bibtex Eintrag [24]

Enhanced Convective Heat Transfer Due To Dynamically Forced Impingement Jets Arrays [25]

Haucke, F. and Nitsche, W.

Proceedings of ASME Turbo Expo: Turbomachinery Technical Conference and Exposition, Seoul, South Korea 2016

Download Bibtex Eintrag [26]

Constrained Repetitive Model Predictive Control Applied to an Compressor Stator Vane Flow [27]

Steinberg, S., Staats, M., Nitsche, W. and King, R.

Proceedings of ASME Turbo Expo: Turbomachinery Technical Conference and Exhibition, Seoul, South Korea 2016

Download Bibtex Eintrag [28]

Experimental Investigations on the Efficiency of Active Flow Control in a Compressor Cascade with Periodic non-steady Outflow Conditions [29]

Staats, M. and Nitsche, W.

Proceedings of ASME Turbo Expo 2017: Turbine Technical Conference and Exposition GT 2017

Download Bibtex Eintrag [30]

ENHANCED CONVECTIVE HEAT TRANSFER DUE TO DYNAMICALLY FORCED IMPINGEMENT JET ARRAYS [31]

Haucke, F., Nitsche, W. and Peitsch, D.

Proceedings of ASME Turbo Expo 2016

Download Bibtex Eintrag [32]

Interaction of wing-tip vortices by coupling of two NACA0021 profiles [33]

Grund, T., Staats, M., Ebert, C. and Weiss, J.

Proceedings of 54th 3AF International Conference on Applied Aerodynamics 2019

Download Bibtex Eintrag [34]

Wing Tip Drag Reduction at Nominal Take-Off Mach Number: An Approach to Local Active Flow Control with a Highly Robust Actuator System [35]

Bauer, M., Grund, T., Nitsche, W. and Ciobaca, V.

Preprints 2016 2016

Download Bibtex Eintrag [36]

On active control of laminar-turbulent transition on two-dimensional wings [37]

Erdmann, R., Pätzold, A., Engert, M., Peltzer, I. and Nitsche, W.

Philosophical Transactions of the Royal Society A: Mathematical,Physical and Engineering Sciences, 1382-1395. 2011

Download Bibtex Eintrag [38]

N

Benefits of Applying Pulsed Jet Actuation on a Vertical Stabilizer [39]

Loeffler, S. and Weiss, J.

Notes on Numerical Fluid Dynamics and Multidisciplinary Design. Springer. 2020

Download Bibtex Eintrag [40]

Experimental Investigation of a Dynamically Forced Impinging Jet Array [41]

Haucke, F. and Berthold, A.

New Results in Numerical and Experimental Fluid Mechanics XI, Notes on Numerical Fluid Mechanics and Multidisciplinary Design 136 2016

Download Bibtex Eintrag [42]

L

Oberflächenmesstechniken zur Strömungsanalyse am Rostocker Leitexperiment [43]

Wolter, A., Berns, A., Dobriloff, C., Leder, A., Obermeier, E. and Nitsche, W.

Proceedings der 15. GALA-Fachtagung "Lasermethoden in der Strömungsmesstechnik". Universitätsbibliothek Rostock, 21.1-21.10. 2007

Download Bibtex Eintrag [44]

J

Infrared based visualizatino of wall shear stress distributions with a hightemporal and spatial resolution [45]

Rudolph, I., Reyer, M. and Nitsche, W.

Journal of Visualization 2007

Download Bibtex Eintrag [46]

Separation Control by Periodic Excitation in a Turbulent Axisymmetric Diffuser Flow [47]

Brunn, A. and Nitsche, W.

Journal of Turbulence 2003

Download Bibtex Eintrag [48]

<< zurück [49]
vor >> [63]
------ Links: ------

Zusatzinformationen / Extras

Direktzugang

Schnellnavigation zur Seite über Nummerneingabe

Copyright TU Berlin 2008