Burkhard Gölling

发表

Robust Closed-Loop Lift Control on an Industry-Relevant Civil Aircraft Half Model

Robert King, Notger Heinz, Burkhard Gölling, 2010 .

Active Flow Separation Control on a High-Lift Wing-Body Configuration Part 2: The Pulsed Blowing Application

Ralf Rudnik, Matthias Bauer, Vlad Ciobaca, 2011 .

Pilot Study of a High Lift Wing Configuration for Performance Optimization

Ralf Rudnik, Wiebke Breitenstein, Vlad Ciobaca, 2010 .

Active Flow-Separation Control on a High-Lift Wing-Body Configuration

Ralf Rudnik, Matthias Bauer, Wiebke Breitenstein, 2013 .

Active Flow Control on an Industry-Relevant Civil Aircraft Half Model

Wolfgang Nitsche, Matthias Bauer, Burkhard Gölling, 2010 .

Dynamic Flow Control Experiments for Innovative High-Lift Configurations on IHK/M-FLY Programs

Jochen Wild, Rolf Radespiel, Christian J. Kähler, 2009 .

Active Flow Separation Control on a High-Lift Wing-Body Configuration - Part 1: Baseline Flow and Constant Blowing

Ralf Rudnik, Wiebke Breitenstein, Vlad Ciobaca, 2011 .

Low noise design trends derived from wind tunnel testing on advanced high-lift devices

Markus Fischer, Hermann Holthusen, Rolf Emunds, 2006 .

C13-002 NASA Standard for Models and Simulations: Philosophy

Edwin R. Galea, Xavier Prats, Joseph H. Morrison, 2013 .

Experimental Investigations of Separating Boundary-Layer Flow from Circular Cylinder at Reynolds Numbers from 105 up to 107 three-dimensional Vortex Flow of a Circular Cylinder)

Burkhard Gölling, 2006 .