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151. Evaluation of Initial Amplitudes of Free-Stream Excited Tollmien-Schlichting Waves from Flight-Test Data

152. Development of a Sensor-Actuator-System for Active Control of Boundary Layer Instabilities in Compressible Flows

153. The Space-Time Expansion DG Method

154. Experimental Investigations of Controlled Transition in a Laminar Separation Bubble at an Axisymmetric Diffuser

155. Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction Using the DLR TAU Code

156. Enhanced Runge-Kutta/Implicit Methods for Solving the Navier-Stokes Equations

157. RANS Simulations with One and Six Degrees of Freedom Rigid Body Motions

158. Direct Numerical Simulation of a Short Laminar Separation Bubble and Early Stages of the Bursting Process

159. Manipulation of Attachment Line Transition by Geometry Modification at the Slat of a Multi-element Airfoil

160. Using CryoTSP as a Tool for Transition Detection and Instability Examination at High Reynolds Numbers

161. The Parallel Mesh Deformation of the DLR TAU-Code

162. Simulation of Oscillating Airfoils and Moving Flaps Employing the DLR-TAU Unsteady Grid Adaptation

163. Adjoint Algorithms for the Optimization of 3d Turbulent Configurations

164. Improvement of the Automatic Grid Adaptation for Vortex Dominated Flows Using Advanced Vortex Indicators with the DLR-Tau Code

165. Three-Dimensional Discontinuous Galerkin Codes to Simulate Viscous Flow by Spatial Discretization of High Order and Curved Elements on Unstructured Grids

166. An Investigation into Internal and External Force Balance Configurations for Short Duration Wind Tunnels

167. Studies of Reynolds Number Effects on Wing Tip Vortex Positions by Means of Laser Light Sheet (LLS) and Background Oriented Schlieren (BOS) Technique Under Cryogenic Conditions

168. Measurement of Unsteady Surface Forces by Means of Piezoelectrical Copolymer Coatings

169. Numerical Simulation of a Wing with a Gapless High-Lift System Using Circulation Control

170. Design of a Retrofit Winglet for a Transport Aircraft with Assessment of Cruise and Ultimate Structural Loads

171. Multiple Discipline Take-Off Weight Minimization for a Supersonic Transport Aircraft

172. Pressure and Heat Flux Measurements on the Surface of a Low-Aspect-Ratio Circular Cylinder Mounted on a Ground Plate

173. Project ForMEx — A New CFD Approach for Transposition of Wind Tunnel Data Towards Flight Conditions

174. Shock Control Bumps on Flexible and Trimmed Transport Aircraft in Transonic Flow

175. A Flat Plate Experiment for Investigations of Vortex Generator Jets at High Reynolds Number

176. Automatic Differentiation of an Entire Design Chain for Aerodynamic Shape Optimization

177. Investigation of Flow Induced Sound Radiated by a Forward Facing Step

178. Application of PIV Techniques for Rotor Blade Tip Vortex Characterization

179. Numerical Investigation of Flow-Induced Noise Generation at the Nozzle End of Jet Engines

180. Numerical Analysis of Sound Generating Mechanisms of a High-Lift Device

181. On the Design of Silent Trailing-Edges

182. URANS and DES Simulation of Flow Around a Rectangular Cylinder

183. Active Manipulation of a Rectangular Wing Vortex Wake with Oscillating Ailerons and Winglet-Integrated Rudders

184. A New Actuator Disk Model for the TAU Code and Application to a Sailplaine with a Folding Engine

185. Numerical Analysis of Wing Vortices

186. Studies on Tailplane Stall for a Generic Transport Aircraft Wind Tunnel Model

187. High-Reynolds-Number Design of a Wing Section Including Control of Boundary Layer Properties

188. An Airbrake Design Methodology for Steep Approaches

189. Development and validation of hybrid grid-based and grid-free computational VπLES method

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