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1 |
Investigation of blunt trailing edge noise from an asymmetric airfoil under different aerodynamic loads
Stahl, Kathrin. - Düren : Shaker, 2023
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2 |
Prediction of laminar-turbulent transition on helicopter rotors in forward flight using the U/RANS solver TAU with an approximate boundary layer method
Heister, Christoph. - Braunschweig : Deutsches Zentrum für Luft- und Raumfahrt e.V., Institut für Aerodynamik und Strömungstechnik, Februar 2016
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3 |
Numerische Untersuchung des Einflusses von stromauf laufenden Druckwellen auf die Transition im Transschall
Hermes, Viktor. - Aachen : Shaker, 2014
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4 |
Unmanned aerial vehicle for flow control experiments with dielectric barrier discharge plasma acctuators
Friedrichs, Wilm, 2014
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5 |
Control of the secondary crossflow instability
Friederich, Tillmann. - Aachen : Shaker, 2013
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6 |
Numerical simulation of aerodynamic plasma actuator effects
Vieira, Débora Gleice da Silva Del Rio, 2013
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7 |
Boundary-layer stabilization with dielectric barrier discharge plasmas for free-flight application
Duchmann, Alexander, 2012
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8 |
Miniaturized piezoelectric actuators for high-speed flow control applications
Bolzmacher, Christian. - Aachen : Shaker, 2011
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9 |
Implementation, verification and validation of empirical transition criteria for airfoil and rotary wing applications using the DLR FLOWer code
Heister, Christoph. - Braunschweig : Dt. Zentrum für Luft- und Raumfahrt, 2010
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