New results in numerical and experimental fluid mechanics VI: contributions to the 15th STAB/DGLR symposium Darmstadt, Germany 2006
Gespeichert in:
Format: | Buch |
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Sprache: | English |
Veröffentlicht: |
Berlin [u.a.]
Springer
2007
|
Schriftenreihe: | Notes on numerical fluid mechanics and multidisciplinary design
96 |
Schlagworte: | |
Online-Zugang: | http://deposit.dnb.de/cgi-bin/dokserv?id=3018363&prov=M&dok_var=1&dok_ext=htm Inhaltsverzeichnis |
Beschreibung: | XIV, 472 S. Ill., graph. Darst. |
ISBN: | 3540744584 9783540744580 |
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Datensatz im Suchindex
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adam_text |
reword
), A D’Alascio (München), J Delfs (Braunschweig), R Eggels
), K Ehrenfried (Göttingen), R Ewert (Braunschweig), M Fischer
R Friedrich (München), R Grundmann (Dresden), P Hakenesch
), H Hansen (Bremen), R Hartmann (Braunschweig), St Hein (Göttingen),
nnecke (Darmstadt), P Hennig (Unterschleißheim), R Hold (München),
el (Weßling), J Kompenhans (Göttingen), G Koppenwallner (Katlenburg-
Kordulla (Noordwijk), E Krämer (Stuttgart), H -P Kreplin (Göttingen),
raunschweig), D Kroner (Freiburg), J Longo (Braunschweig), A Meister
F Menter (Otterfing), V Mikulla (München), C -D Munz (Stuttgart),
tzke (Bremen), W Nitsche (Berlin), H Olivier (Aachen), R Radespiel
weig), H -J Rath (Bremen), K Richter (Göttingen), U Rist (Stuttgart),
ann (Göttingen), G Schrauf (Bremen), W Schröder (Aachen), F Seiler
is), J Sesterhenn (München), J Seume (Hannover), P Thiede (Bremen),
ck (Berlin), C Tropea (Darmstadt), R Voß (Göttingen), C Wagner
), C Weiland (München), C Weishäupl (München) and W Würz
eless, the authors sign responsible for the contents of their contributions,
tors are grateful to Prof Dr E H Hirschel as the General Editor of the
Numerical Fluid Mechanics and Multidisciplinary Design and to the
erlag for the opportunity to publish the results of the Symposium
C Tropea, Darmstadt
S Jakirlic, Darmstadt
H -J Heinemann, Göttingen
R Henke, Bremen
H Hönlinger, Göttingen
Table of Contents
Airplane Aerodynamics
An Airbrake Design Methodology for Steep Approaches
B Anil Mertol 1
1
’ High-Reynolds-Number Design of a Wing Section Including Control
' of Boundary Layer Properties
K- Richter, S Koch, H Rosemann 9
■ Numerical Analysis of Wing Vortices
i f Zurheide, W Schröder 17
' Studies on Tailplane Stall for a Generic Transport Aircraft
Wind Tunnel Model
„ A Grote, R Rade spiel 26
URANS and DES Simulation of Flow Around a Rectangular Cylinder
* C Mannini, A Soda, R Voß, G Schewe 36
, Active Manipulation of a Rectangular Wing Vortex Wake with Oscillating
• Ailerons and Winglet-Integrated Rudders
j R Hömschemeyer, C Rixen, S Kauertz, G Neuwerth,
; R Henke 44
A New Actuator Disk Model for the TAU Code and Application to a Sailplane
- with a Folding Engine
A Raichle, S Melber-Wilkending, J Mimisch 52
Design of a Retrofit Winglet for a Transport Aircraft with Assessment
of Cruise and Ultimate Structural Loads
, Th Streit, J Himisch, R Heinrich, B Nagel, K H Horstmann, C Liersch 62
Flow Control
Numerical Simulation of a Wing with a Gapless High-Lift System Using
Circulation Control
K -C Pfingsten, R Radespiel
71
X
Table of Contents
Shock Control Bumps on Flexible and Trimmed Transport Aircraft
in Transonic Flow
B König, M Pätzhold, T Lutz, E Krämer 80
A Flat Plate Experiment for Investigations of Vortex Generator Jets at High
Reynolds Number
J Ortmanns, C J Kühler, R Rade spiel 88
Experimental Simulation and Test Techniques
Measurement of Unsteady Surface Forces by Means of Piezoelectrical
Copolymer Coatings
J Domhardt, J Leuckert, / Peltzer, VF Nitsche 96
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
D Pallek, F Klinge 104
Project ForMEx - A New CFD Approach for Transposition of Wind Tunnel
Data Towards Flight Conditions
5 Melber-Wilkending, G Wichmann 113
Pressure and Heat Flux Measurements on the Surface of a Low-Aspect-Ratio
Circular Cylinder Mounted on a Ground Plate
T Rödiger, H Knauss, U Gaisbauer, E Krämer 121
An Investigation into Internal and External Force Balance Configurations
for Short Duration Wind Tunnels
M Robinson, J Martinez Schramm, K Hannemann 129
Numerics
Multiple Discipline Take-Off Weight Minimization for a Supersonic
Transport Aircraft
U Herrmann 137
Three-Dimensional Discontinous Galerkin Codes to Simulate Viscous Flow
by Spatial Discretization of High Order and Curved Elements on
Unstructured Grids
C Lübon, S Wagner 145
The Space-Time Expansion DG Method
F Lärcher, G Gassner, C -D Munz 154
The Parallel Mesh Deformation of the DLR TAU-Code
T Gerhold, J Neumann 162
Table of Contents
XI
le of Contents
trol Bumps on Flexible and Trimmed Transport Aircraft
c Flow
Pätzhold, T Lutz, E Krämer 80
Experiment for Investigations of Vortex Generator Jets at High
umber
s, C J Kühler, R Radespiel 88
ntal Simulation and Test Techniques
nt of Unsteady Surface Forces by Means of Piezoelectrical
Coatings
t, J Leuckert, I Peltzer, W Nitsche 96
eynolds Number Effects on Wing Tip Vortex Positions by Means
‘ght Sheet (LLS) and Background Oriented Schlieren (BOS)
Under Cryogenic Conditions
Klinge 104
rMEx - A New CFD Approach for Transposition of Wind Tunnel
rds Flight Conditions
ilkending, G Wichmann 113
d Heat Flux Measurements on the Surface of a Low-Aspect-Ratio
ylinder Mounted on a Ground Plate
H Knauss, U Gaisbauer, E Krämer 121
gation into Internal and External Force Balance Configurations
uration Wind Tunnels
n, J Martinez Schramm, K Hannemann 129
S
iscipline Take-Off Weight Minimization for a Supersonic
Aircraft
nn 137
ensional Discontinous Galerkin Codes to Simulate Viscous Flow
Discretization of High Order and Curved Elements on
red Grids
S Wagner 145
-Time Expansion DG Method
, G Gassner, C -D Munz 154
162
* ulation of Oscillating Airfoils and Moving Flaps Employing
the DLR-TAU Unsteady Grid Adaptation
' D Gardner, K Richter, H Rosemann 170
;RANS Simulations with One and Six Degrees of Freedom
4|Ugid Body Motions
3* Schwarz 178
Improvement of the Automatic Grid Adaptation for Vortex Dominated
Plows Using Advanced Vortex Indicators with the DLR-Tau Code
M Widhalm, A Schütte, T Alrutz, M Orlt 186
Adjoint Algorithms for the Optimization of 3d Turbulent Configurations
P Dwight, J Brezillon 194
Enhanced Runge-Kutta/Implicit Methods for Solving the Navier-Stokes
lEquations
fC -C Rossow 202
Laminar Flow Control and Transition
/Navier-Stokes High-Lift Airfoil Computations with Automatic Transition
Prediction Using the DLR TAU Code
■A Krumbein, N Krimmelbein , 210
Manipulation of Attachment Line Transition by Geometry Modification
at the Slat of a Multi-element Airfoil
'*/ Wild, H Dettmar 219
• - Using CryoTSP as a Tool for Transition Detection and Instability
Examination at High Reynolds Numbers
\ V Fey, Y Egami, C Klein 227
-m: '
Direct Numerical Simulation of a Short Laminar Separation Bubble
': amp;nd Early Stages of the Bursting Process
“Ö Marxen, D Henningson 235
Experimental Investigations of Controlled Transition in a Laminar
Reparation Bubble at an Axisymmetric Diffuser
L Hoefener, W Nitsche 244
• Development of a Sensor-Actuator-System for Active Control of Boundary
Layer Instabilities in Compressible Flows
■ M Engert, A Pätzold, W Nitsche 252
Evaluation of Initial Amplitudes of Free-Stream Excited Tollmien-Schlichting
»Waves from Flight-Test Data
'jA Seitz
lei Mesh Deformation of the DLR TAU-Code
, J Neumann
260
XII
Table of Contents
The Role of Turbulent Dissipation for Flow Control of Near-Wall
Turbulence
B Frohnapfel, P hammers, J Jovanovic 268
Hypersonic Flows
Radical Farming in Scramjets
J Odam, A Pauli 276
Aerothermodynamic Investigation of the Pre-X Configuration in HEG
J Martinez Schramm, B Reimann 284
SHEFEX - A First Aerodynamic Post-flight Analysis
T Barth, T Eggers 291
Simulation of Magnetohydrodynamic Effects on an Ionised Hypersonic
Flow by Using the TAU Code
C Böttcher, V Hannemann, H Liideke 300
Heat Fluxes Inside a Cavity Placed at the Nose of a Projectile Measured
in a Shock Tunnel at Mach 4 5
F Seiler, J Srulijes, M Gimenez Pastor, P Mangold 309
Experimental Investigation and Numerical Simulation on a Missile Radome
at Mach 6
C Dankert, H Otto 317
Turbomachines
Control of Flow Separation in Adverse Pressure Gradients by Means
of Crosswise Grooved Surfaces for Turbo Machine Applications
W Hage, R Meyer, C O Paschereit 324
Wave Drag Reduction Approach for Lattice Wings at High Speeds
E Schiilein, D Guyot 332
Forces and Velocity Measurements in Ship Propulsion Systems
J Pego, H Lienhart, F Durst, K Tigges 340
Flows Past Bodies
Numerical Simulation of the Flow Around a Finite Cylinder with Ground
Plate in Comparison to Experimental Measurements
O Frederich, E Wassen, F Thiele, M Jensch,
M Brede, F Hiittmann, A Leder
348
Table of Contents
XUI
le of Contents
Turbulent Dissipation for Flow Control of Near-Wall
el, P Lammers, J Jovanovic 268
ic Flows
ming in Scramjets
Pauli 276
odynamic Investigation of the Pre-X Configuration in HEG
Schramm, B Reimann 284
A First Aerodynamic Post-flight Analysis
Eggers 291
of Magnetohydrodynamic Effects on an Ionised Hypersonic
ing the TAU Code
V Hannemann, H Liideke 300
Inside a Cavity Placed at the Nose of a Projectile Measured
Tunnel at Mach 4 5
Srulijes, M Gimenez Pastor, P Mangold 309
tal Investigation and Numerical Simulation on a Missile Radome
H Otto 317
chines
Flow Separation in Adverse Pressure Gradients by Means
Grooved Surfaces for Turbo Machine Applications
Meyer, C O Paschereit 324
Reduction Approach for Lattice Wings at High Speeds
D Guyot 332
Velocity Measurements in Ship Propulsion Systems
Lienhart, F Durst, K Tigges 340
t Bodies
Simulation of the Flow Around a Finite Cylinder with Ground
mparison to Experimental Measurements
h, E Wassen, F Thiele, M Jensch,
Hiittmann, A Leder 348
umerical Simulation of Aerodynamic Problems with SSG/LRR-co Reynolds
ess Turbulence Model Using the Unstructured TAU Code
, jEisfeld 356
* umerical Simulation of the Flow Field Around the Stratospheric
bservatory for Infrared Astronomy
r Schmid, T Lutz, E Krämer 364
* rge Eddy Simulation / Direct Numerical Simulation
' S of Compressible Inert and Infinitely Fast Reacting Mixing Layers
‘ Mahle, J Sesterhenn, R Friedrich 372
velopment of a Numerical Procedure for Direct Simulations of Turbulent
önvection in a Closed Rectangular Cell
Karczorowski, A Shishkin, O Shishkina, C Wagner 381
mputation of Supersonic Base Flow Using Detached Eddy Simulation
X Togiti, H Liideke 389
rge-Eddy Simulation of Tundish Flows Using Preconditioning
X Alkishriwi, M Meinke, W Schröder 397
umerical Investigation of Effusion Cooling in Hypersonic
' undary-Layer Flow
, Linn, MJ Kloker 405
eroacoustics
umerical Investigation of Flow-Induced Noise Generation
t the Nozzle End of Jet Engines
Babucke, M J Kloker, U Rist 413
Umerical Analysis of Sound Generating Mechanisms of a High-Lift
vice
König, W Schroder, M Meinke 421
v the Design of Silent Trailing-Edges
- Herr 430
vestigation of Flow Induced Sound Radiated by a Forward Facing Step
Hahn, S Becker, I Ali, M Escobar, M Kaltenbacher 438
‘scellaneous
a pplication of PIV Techniques for Rotor Blade Tip Vortex
racterization
, Richard, B G Van der Wall, M Raffel, M Thimm
446
XIV Table of Contents
Automatic Differentiation of an Entire Design Chain for Aerodynamic
Shape Optimization
N R Gauger, A Walther, C Moldenhauer, M Widhalm 454
Computational Study of Mean Flow and Turbulence Structure in Inflow
System of a Swirl Combustor
S Saric, S Jakirlic, D Cavar, B Kniesner, P Altenhöfer,
C Tropea 462
Author Index |
any_adam_object | 1 |
author_GND | (DE-588)110256468 |
building | Verbundindex |
bvnumber | BV035367332 |
ctrlnum | (OCoLC)254896557 (DE-599)DNB986189405 |
dewey-full | 629.1323 620 |
dewey-hundreds | 600 - Technology (Applied sciences) |
dewey-ones | 629 - Other branches of engineering 620 - Engineering and allied operations |
dewey-raw | 629.1323 620 |
dewey-search | 629.1323 620 |
dewey-sort | 3629.1323 |
dewey-tens | 620 - Engineering and allied operations |
discipline | Verkehr / Transport |
format | Book |
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genre | (DE-588)1071861417 Konferenzschrift 2006 Darmstadt gnd-content |
genre_facet | Konferenzschrift 2006 Darmstadt |
id | DE-604.BV035367332 |
illustrated | Illustrated |
indexdate | 2024-07-20T10:05:23Z |
institution | BVB |
institution_GND | (DE-588)6069784-2 (DE-588)5094329-7 |
isbn | 3540744584 9783540744580 |
language | English |
lccn | 2007934013 |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-017171279 |
oclc_num | 254896557 |
open_access_boolean | |
owner | DE-210 DE-634 |
owner_facet | DE-210 DE-634 |
physical | XIV, 472 S. Ill., graph. Darst. |
publishDate | 2007 |
publishDateSearch | 2007 |
publishDateSort | 2007 |
publisher | Springer |
record_format | marc |
series | Notes on numerical fluid mechanics and multidisciplinary design |
series2 | Notes on numerical fluid mechanics and multidisciplinary design |
spelling | New results in numerical and experimental fluid mechanics VI contributions to the 15th STAB/DGLR symposium Darmstadt, Germany 2006 Cameron Tropea ... (eds.) Berlin [u.a.] Springer 2007 XIV, 472 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Notes on numerical fluid mechanics and multidisciplinary design 96 Aerodynamics / Congresses Airplanes / Design and construction / Congresses Fluid dynamics / Congresses Turbulence / Congresses Mehrfeldproblem (DE-588)7544635-2 gnd rswk-swf Optimierungsproblem (DE-588)4390818-4 gnd rswk-swf Numerische Strömungssimulation (DE-588)4690080-9 gnd rswk-swf Flugzeugaerodynamik (DE-588)4135410-2 gnd rswk-swf Entwurf (DE-588)4121208-3 gnd rswk-swf Numerisches Verfahren (DE-588)4128130-5 gnd rswk-swf Flugzeug (DE-588)4017672-1 gnd rswk-swf Strömungsmechanik (DE-588)4077970-1 gnd rswk-swf (DE-588)1071861417 Konferenzschrift 2006 Darmstadt gnd-content Flugzeugaerodynamik (DE-588)4135410-2 s DE-604 Strömungsmechanik (DE-588)4077970-1 s Numerisches Verfahren (DE-588)4128130-5 s Numerische Strömungssimulation (DE-588)4690080-9 s Flugzeug (DE-588)4017672-1 s Entwurf (DE-588)4121208-3 s Mehrfeldproblem (DE-588)7544635-2 s Optimierungsproblem (DE-588)4390818-4 s Tropea, Cameron 1954- Sonstige (DE-588)110256468 oth Deutsche Strömungsmechanische Arbeitsgemeinschaft Sonstige (DE-588)6069784-2 oth Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth Sonstige (DE-588)5094329-7 oth Notes on numerical fluid mechanics and multidisciplinary design 96 (DE-604)BV014762175 96 http://deposit.dnb.de/cgi-bin/dokserv?id=3018363&prov=M&dok_var=1&dok_ext=htm HEBIS Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=017171279&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
spellingShingle | New results in numerical and experimental fluid mechanics VI contributions to the 15th STAB/DGLR symposium Darmstadt, Germany 2006 Notes on numerical fluid mechanics and multidisciplinary design Aerodynamics / Congresses Airplanes / Design and construction / Congresses Fluid dynamics / Congresses Turbulence / Congresses Mehrfeldproblem (DE-588)7544635-2 gnd Optimierungsproblem (DE-588)4390818-4 gnd Numerische Strömungssimulation (DE-588)4690080-9 gnd Flugzeugaerodynamik (DE-588)4135410-2 gnd Entwurf (DE-588)4121208-3 gnd Numerisches Verfahren (DE-588)4128130-5 gnd Flugzeug (DE-588)4017672-1 gnd Strömungsmechanik (DE-588)4077970-1 gnd |
subject_GND | (DE-588)7544635-2 (DE-588)4390818-4 (DE-588)4690080-9 (DE-588)4135410-2 (DE-588)4121208-3 (DE-588)4128130-5 (DE-588)4017672-1 (DE-588)4077970-1 (DE-588)1071861417 |
title | New results in numerical and experimental fluid mechanics VI contributions to the 15th STAB/DGLR symposium Darmstadt, Germany 2006 |
title_auth | New results in numerical and experimental fluid mechanics VI contributions to the 15th STAB/DGLR symposium Darmstadt, Germany 2006 |
title_exact_search | New results in numerical and experimental fluid mechanics VI contributions to the 15th STAB/DGLR symposium Darmstadt, Germany 2006 |
title_full | New results in numerical and experimental fluid mechanics VI contributions to the 15th STAB/DGLR symposium Darmstadt, Germany 2006 Cameron Tropea ... (eds.) |
title_fullStr | New results in numerical and experimental fluid mechanics VI contributions to the 15th STAB/DGLR symposium Darmstadt, Germany 2006 Cameron Tropea ... (eds.) |
title_full_unstemmed | New results in numerical and experimental fluid mechanics VI contributions to the 15th STAB/DGLR symposium Darmstadt, Germany 2006 Cameron Tropea ... (eds.) |
title_short | New results in numerical and experimental fluid mechanics VI |
title_sort | new results in numerical and experimental fluid mechanics vi contributions to the 15th stab dglr symposium darmstadt germany 2006 |
title_sub | contributions to the 15th STAB/DGLR symposium Darmstadt, Germany 2006 |
topic | Aerodynamics / Congresses Airplanes / Design and construction / Congresses Fluid dynamics / Congresses Turbulence / Congresses Mehrfeldproblem (DE-588)7544635-2 gnd Optimierungsproblem (DE-588)4390818-4 gnd Numerische Strömungssimulation (DE-588)4690080-9 gnd Flugzeugaerodynamik (DE-588)4135410-2 gnd Entwurf (DE-588)4121208-3 gnd Numerisches Verfahren (DE-588)4128130-5 gnd Flugzeug (DE-588)4017672-1 gnd Strömungsmechanik (DE-588)4077970-1 gnd |
topic_facet | Aerodynamics / Congresses Airplanes / Design and construction / Congresses Fluid dynamics / Congresses Turbulence / Congresses Mehrfeldproblem Optimierungsproblem Numerische Strömungssimulation Flugzeugaerodynamik Entwurf Numerisches Verfahren Flugzeug Strömungsmechanik Konferenzschrift 2006 Darmstadt |
url | http://deposit.dnb.de/cgi-bin/dokserv?id=3018363&prov=M&dok_var=1&dok_ext=htm http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=017171279&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
volume_link | (DE-604)BV014762175 |
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