《New Results in Numerical and Experimental Fluid Mechanics》第十辑

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《New Results in Numerical and Experimental Fluid Mechanics X: Contributions to the 19th STAB/DGLR Symposium Munich, Germany, 2014》
数值和实验流体力学的新结果第十辑：第19届STAB / DGLR研讨会的贡献，德国慕尼黑2014年
编者：
Andreas Dillmann
Gerd Heller
Ewald Krämer
Claus Wagner
Christian Breitsamter
出版社：Springer
出版时间：2016年


目录
Part I Airplane Aerodynamics/Propulsion Integration
Numerical Stall Behavior Investigation of an Aircraft
Equipped with Coanda Flap and Droop Nose. . . . . . . . . . . . . . . . . . . . 3
Marco Burnazzi, Jakob Thiemeier and Rolf Radespiel
Aerodynamic Design of a Folded Krüger Device
for a HLFC Wing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
Dirk M. Franke and Jochen Wild
Validation of CFD Airdrop Simulations in the Vortical
Wake of an Aircraft with Open Ramp . . . . . . . . . . . . . . . . . . . . . . . . . 29
Sven Geisbauer and Hauke Schmidt
Numerical Investigation of Unsteady Tangential Blowing
at the Rudder of a Vertical Tailplane Airfoil . . . . . . . . . . . . . . . . . . . . 39
Anna Kröhnert
Propeller and Active High Lift Wing Interaction
in Experiment and Simulation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 51
Carsten Lenfers, Nils Beck and Marc Bauer
Sensitivity of a Low Pressure Ratio Jet Engine Fan
to Inlet Distortion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 63
Marius Theune, Dirk Schönweitz and Rainer Schnell
Part II Optimization
A Consistent and Robust Discrete Adjoint Solver for the SU2
Framework—Validation and Application . . . . . . . . . . . . . . . . . . . . . . . 77
Tim Albring, Max Sagebaum and Nicolas R. Gauger
ix
Comparison of Breguet and ODE Evaluation of the Cruise
Mission Segment in the Context of High-Fidelity Aircraft MDO . . . . . . 87
Časlav Ilić, Tanja Führer, Nagaraj Banavara, Mohammad Abu-Zurayk,
Gunnar Einarsson, Martin Kruse, Jan Himisch, Doreen Seider
and Richard-Gregor Becker
Part III Turbulence Research and Turbulence Modeling
Control of the Secondary Crossflow Instability Using Plasma
Actuators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 101
Philipp C. Dörr and Markus J. Kloker
On Phase Asymmetries in Oscillatory Pipe Flow. . . . . . . . . . . . . . . . . . 113
Daniel Feldmann and Claus Wagner
Generalized Energy Budget Equations for Large-Eddy
Simulations of Scalar Turbulence. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 123
Michael Gauding, Achim Wick, Jens Henrik Goebbert,
Markus Hempel, Norbert Peters and Christian Hasse
Statistical Description of Streamline Segments in a Turbulent
Channel Flow with a Wavy Wall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 135
Fabian Hennig, Jonas Boschung and Norbert Peters
Application of Numerical Wall Functions for Boundary
Layer Flows with Separation and Reattachment. . . . . . . . . . . . . . . . . . 145
Tobias Knopp, Fabian Spallek, Octavian Frederich
and Gerd Rapin
Simulation of a Helicopter Engine Jet Including a Realistic
Nozzle Geometry. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 157
Mehmet Onur Cetin, Matthias Meinke and Wolfgang Schröder
Large-Eddy Simulation of the Flow Field in a Rotating Axial Fan. . . . . 167
Alexej Pogorelov, Matthias Meinke and Wolfgang Schröder
Investigation of the Law-of-the-Wall for a Turbulent
Boundary Layer Flow Subject to an Adverse Pressure
Gradient Using Particle Imaging . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 177
Tobias Knopp, Nicolas A. Buchmann, Daniel Schanz,
Christian Cierpka, Rainer Hain, Andreas Schröder
and Christian J. Kähler
Part IV Laminar Flow Control and Transition
Numerical Investigation of the Bending of Slender Wall-Mounted
Cylinders in Low Reynolds Number Flow . . . . . . . . . . . . . . . . . . . . . . 191
Gabriel Axtmann, Ulrich Rist, Franziska Hegner
and Christoph Bruecker
x Contents
Effect of Forward-Facing Steps on Boundary Layer Transition
at a Subsonic Mach Number . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 203
Marco Costantini, Steffen Risius, Christian Klein
and Winfried Kühn
Combined Active Separation Control on the Leading Edge
and on the Trailing Edge Flap of a Slatless High-Lift
Configuration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 215
Frank Haucke, Matthias Bauer and Wolfgang Nitsche
Receptivity of a Swept-Wing Boundary Layer to Steady
Vortical Free-Stream Disturbances. . . . . . . . . . . . . . . . . . . . . . . . . . . . 227
Holger B.E. Kurz and Markus J. Kloker
Discrete Adjoint Based Optimal Active Control of Separation
on a Realistic High-Lift Configuration . . . . . . . . . . . . . . . . . . . . . . . . . 237
Anil Nemili, Emre Özkaya, Nicolas R. Gauger, Felix Kramer
and Frank Thiele
Nonlinear Disturbance Evolution Downstream of a Medium
Height Roughness Element . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 247
Benjamin Plogmann, Werner Würz and Ewald Krämer
Leading-Edge Receptivity to Free-Stream Vorticity
of Streamwise Corner-Flow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 259
Oliver T. Schmidt, Jennifer Staudenmeyer, Ulrich Rist
and Claus-Dieter Munz
IR Measurements for Quantification of Laminar Boundary
Layer Stabilization with DBD Plasma Actuators. . . . . . . . . . . . . . . . . . 269
Bernhard Simon, Paul Schnabel and Sven Grundmann
Local Stability Analysis of Laminar-Turbulent Boundary Layer
Transition on Blunt Generic Re-Entry Capsules . . . . . . . . . . . . . . . . . . 279
Alexander Theiss, Martin Lichtmes and Stefan Hein
Part V Rotorcraft Aerodynamics
Transition Determination on a Periodic Pitching Airfoil
Using Phase Averaging of Pressure Data . . . . . . . . . . . . . . . . . . . . . . . 291
A.D. Gardner and K. Richter
Validation of a Flow Simulation for a Helicopter Fuselage
Including a Rotating Rotor Head. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 303
Moritz Grawunder, Roman Reß, Victor Stein, Christian Breitsamter
and Nikolaus A. Adams
Contents xi
Comparison Between Two-Dimensional and Three-Dimensional
Dynamic Stall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 315
K. Kaufmann, A.D. Gardner and M. Costes
CFD/CSD Trim Coupled Simulation of the HART II Rotor
with Higher Harmonic Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 327
Annika Länger
Experimental Investigation of Dynamic Stall on a Pitching
Rotor Blade Tip . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 339
Christoph B. Merz, C. Christian Wolf, Kai Richter, Kurt Kaufmann
and Markus Raffel
Influence of Periodically Varying Incident Velocity
on the Application of Semi-Empirical Dynamic Stall Models . . . . . . . . . 349
Dominik Schicker and Manfred Hajek
Coupled Fluid-Structure Simulations of a Trimmed Helicopter
Rotor in Forward Flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 359
S. Surrey, J.-H. Wendisch and F. Wienke
Part VI Technical Flows
Transient Temperature Fields of Turbulent Mixed Convection
in an Aircraft Cabin Caused by a Local Heat Source . . . . . . . . . . . . . . 371
T. Dehne and J. Bosbach
Numerical Simulation of the Thermal Comfort in a Model
of a Passenger Car Cabin . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 383
Mikhail Konstantinov and Claus Wagner
Part VII Vehicle Aerodynamics
Rear-End Shape Influence on the Aerodynamic Properties
of a Realistic Car Model: A RANS and Hybrid LES/RANS Study. . . . . 397
S. Jakirlic, L. Kutej, D. Hanssmann, B. Basara, T. Schütz and C. Tropea
Adjoint-Based, CAD-Free Aerodynamic Shape Optimization
of High-Speed Trains . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 409
Daria Jakubek and Claus Wagner
Large Eddy Simulations of Side Flow Past a Generic Model
of a High-Speed Train. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 421
Natalia Kin, Ralf Deiterding and Claus Wagner
Flow Field Analysis of a Detailed Road Vehicle Model
Based on Numerical Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 433
Robin Placzek and Peter Scholz
xii Contents
Part VIII Aeroelasticity and Structural Dynamics
Flutter Prediction of a Laminar Airfoil Using a Doublet Lattice
Method Corrected by Experimental Data. . . . . . . . . . . . . . . . . . . . . . . 445
Anne Hebler and Reik Thormann
Numerical Modeling of Wind Tunnel Walls for the Investigation
of Oscillating Airfoils . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 457
Christoph Kaiser and Jens Nitzsche
Efficient Modeling of Generalized Aerodynamic Forces
Across Mach Regimes Using Neuro-Fuzzy Approaches . . . . . . . . . . . . . 467
Maximilian Winter and Christian Breitsamter
Part IX Numerical Simulation / Aerodynamics
Numerical Simulation of Vortex Roll-Up Processes
Using the SSG/LRR-x Model . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 481
Sebastian Braun, Anna Uhl, Bernhard Eisfeld and Eike Stumpf
Numerical Aero-Structural Dynamic Simulations
of the ASDMAD Wing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 493
Manuel Brüderlin, Bernd Stickan, Bernd Schulze and Marek Behr
Large Eddy Simulation of Turbulent Thermal Convection
Using Different Subgrid-Scale Models . . . . . . . . . . . . . . . . . . . . . . . . . 505
Tomasz Czarnota, Tim Wetzel and Claus Wagner
Highly Resolved Simulations of Turbulent Mixed Convection
in a Vertical Plane Channel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 515
Christian Kath and Claus Wagner
Computer Aided Analysis of Preconditioned Multistage
Runge-Kutta Methods Applied to Solve the Compressible
Reynolds Averaged Navier-Stokes Equations . . . . . . . . . . . . . . . . . . . . 525
Stefan Langer
Adjoint-Based Error Estimation and Mesh Refinement
in an Adjoint-Based Airfoil Shape Optimization of a Transonic
Benchmark Problem . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 537
Ding Li and Ralf Hartmann
Ramifications of Implicit Runge-Kutta Time Integration Scheme. . . . . . 547
Cord-Christian Rossow
Hybrid LES–URANS Methodology for Wall–Bounded Flows
with Synthetic Turbulent Inflow Conditions . . . . . . . . . . . . . . . . . . . . . 561
Stephan Schmidt and Michael Breuer
Contents xiii
A Mesh-Free Parallel Moving Least-Squares-based Interpolation
Method for the Application in Aeroelastic Simulations
With the Flow Simulator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 573
Andreas Schuster, Lars Reimer and Jens Neumann
Development of a Fully Automatic Chimera Hole Cutting
Procedure in the DLR TAU Code . . . . . . . . . . . . . . . . . . . . . . . . . . . . 585
Frank Spiering
Towards the Simulation of Trimmed Flight Conditions
with Active Engines. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 597
Arthur Stück and Ralf Heinrich
Wall Modeled Large Eddy Simulation of a Delta Wing
with Round Leading Edge. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 607
Christian Zwerger, Stefan Hickel, Christian Breitsamter
and Nikolaus Adams
Part X Experimental Aerodynamics / Experimental Simulation
and Test Techniques
Rotating Camera System for In-Flight Propeller Blade
Deformation Measurements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 619
Fritz Boden and Bolesław Stasicki
Fan Blade Deformation Measurements on the DLR Airbus
A320-ATRA by Means of IPCT as Part of the Ground Test
Campaign in the Frame of the DLR-project SAMURAI . . . . . . . . . . . . 629
Tania Kirmse, Sandra Maring, Paul-Benjamin Ebel
and Andreas Schröder
Experimental Investigation of Periodically Generated Vortex
Rings in Crossflow Impinging on a Flat Plate. . . . . . . . . . . . . . . . . . . . 639
Henning Kroll, Armin Weiss and Wolfgang Nitsche
Experimental Determination of Dynamic Derivatives in a Wind
Tunnel Using Parameter Identification. . . . . . . . . . . . . . . . . . . . . . . . . 651
Thomas Loeser and Detlef Rohlf
Development of a Rotor Test Facility for the Investigation
of Dynamic Stall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 663
Till Schwermer, Kai Richter and Markus Raffel
Influence of the Shear Layer Thickness on the Flow Around
Unsteady Airfoils . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 675
Alexander Widmann and Cameron Tropea
xiv Contents
Part XI Aeroacoustics
Towards an Impact-Based Noise Reduction Method
for Conceptual Aircraft Design . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 687
Jason Blinstrub and Lothar Bertsch
Overset DNS with Application to Homogeneous Decaying
Turbulence . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 699
R.A.D. Akkermans, N. Buchmann, J. Dierke and R. Ewert
Direct Numerical Simulation of Tonal Noise in Suband
Transonic Airfoil Flow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 709
Manuel A. Gageik, Igor Klioutchnikov and Herbert Olivier
Numerical Simulation of Turbulence Induced Flow Noise in
Automotive Exhaust Systems Using Scale-Resolving
Turbulence Models . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 719
Jan Hillenbrand, Stefan Becker, Thomas Sailer, Martin Wetzel
and Oliver Hausner
Flap Side-Edge Noise Prediction Within Conceptual
Aircraft Design . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 731
M.R. Ramdjanbeg, L. Bertsch, K.-S. Rossignol and D.G. Simons
A Hybrid Discontinuous Galerkin-Finite Volume Method
for Computational Aeroacoustics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 743
Michael Schlottke-Lakemper, Matthias Meinke
and Wolfgang Schröder
Identification of Sound Sources in Ducted Flows
with an LES-SI-DMD Approach: Influence of Mesh Refinement
and Subgrid Scale Models . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 755
Carlo Sovardi and Wolfgang Polifke
Flow-Induced Noise of a Forward-Backward Facing Step . . . . . . . . . . . 767
Matthias Springer, Christoph Scheit and Stefan Becker
Experimental Investigations of Tonal Noise on a Vehicle
Side Mirror . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 777
Maike Werner, Werner Würz and Ewald Krämer
Towards Adjoint-Based Trailing-Edge Noise Minimization
Using Porous Material. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 789
Beckett Y. Zhou, Nicolas R. Gauger, Seong R. Koh, Matthias Meinke
and Wolfgang Schröder
Contents xv
Part XII Hypersonic Aerodynamics
Numerical Simulation of the Flow and Combustion Inside
the Reaction Chamber of the AHRES Hybrid Rocket Engine . . . . . . . . 801
Stefan May and Ognjan Božić
Interaction of Acoustic and Entropy Waves with Shocks. . . . . . . . . . . . 811
Thomas Schilden, Matthias Meinke and Wolfgang Schröder
Part XIII High-Agility Configuration
Dynamic Actuation for Delta Wing Post Stall Flow Control . . . . . . . . . 823
Anja Kölzsch, Sophie Blanchard and Christian Breitsamter
CFD Study on a Pitching Missile with Respect to Reduce
the Phantom Yaw Effect . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 833
Christian Schnepf and Erich Schülein
Part XIV Wind Energy
An Adaptive Lattice Boltzmann Method for Predicting
Wake Fields Behind Wind Turbines . . . . . . . . . . . . . . . . . . . . . . . . . . 845
Ralf Deiterding and Stephen L. Wood
Aerodynamic Design and Optimization of a High-Lift Device
for a Wind Turbine Airfoil . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 859
Ana Manso Jaume and Jochen Wild
Investigations on the Wake Development of the MEXICO
Rotor Considering Different Inflow Conditions . . . . . . . . . . . . . . . . . . . 871
Christoph Schulz, Konrad Meister, Thorsten Lutz and Ewald Krämer
Stroke-Wing Engine with Dual Wings for Extracting Power
from an Airstream . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 883
Wolfgang Send
Author Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 895

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