New results in numerical and experimental fluid mechanics II: contributions to the 11th AG STAB DGLR Symposium, Berlin, Germany, 1998
Gespeichert in:
| Format: | Buch |
|---|---|
| Sprache: | English |
| Veröffentlicht: |
Braunschweig
Vieweg
1999
|
| Schriftenreihe: | Notes on numerical fluid mechanics
72 |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | 536 S. graph. Darst. |
| ISBN: | 3528031220 |
Internformat
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| adam_text | IMAGE 1
NEW RESULTS IN NUMERICAL AND EXPERIMENTALFLUIDMECHANICSII
CONTRIBUTIONS TO THE 11TH AG STAB/DGLR SYMPOSIUM BERLIN, GERMANY 1998
EDITED BY WOLFGANG NITSCHE HANS-JOACHIM HEINEMANN AND REINHARD HILBIG
VIEWEG
IMAGE 2
CONTENTS
PAGE
C. ABEGG, H. BIPPES, F.P. BERTOLOTTI: ON THE APPLICATION OF SUCTION FOR
THE STABILIZATION OFCROSSFLOW INSTABILITY OVER PERFORATED WALLS 1
R. ALEWELT: IMPACT OFSTRINGER-WIDTHON THE EFFECT OFHYBRID LAMINAR FLOW
WITH SUCTION.. 8
V. BADER, F.-R. GROSCHE: CONTROL OFFLOW SEPARATION BY DYNAMIC EXITATION
OFTHE FREE SHEAR LAYER 16
M. BAUMANN, D. STURZEBECHER, W. NTTSCHE: ON ACTIVE CONTROL OFBOUNDARY
LAYER INSTABILITIES ON A WING 22
S. BECKER, F.DURST, H. LIENHART: IN-FLIGHT BOUNDARY LAYER
INVESTIGATIONSON A LAMINAR WING USING LASER DOPPLERANEMOMETRY 30
H. BIELER, R. ALEWELT: EFFECT OFMEAN FLOW ACCURACYONPSE RESULTS 37
J. BIRKEMEYER: ADAPTED WINDTUNNEL WALLS FOR A SWEPT WING EXPERIMENT 44
R.C. BLASCHKE, D. HUMMEL: EXPERIMENTAL AND NUMERICAL INVESTIGATIONS ON A
WAVERIDER CONFIGURATION IN INCOMPRESSIBLE FLOW 52
G.BONFIGLI, M.KLOKER: SPATIAL NAVIER-STOKES SIMULATION OF
CROSSFLOW-INDUCED TRANSITION IN A THREE-DIMENSIONALBOUNDARY LAYER 61
C. BREITSAMTER: STRAKE EFFECTS ON THE TURBULENT FIN FLOWFIELD OFA
HIGH-PERFORMANCE FIGHTER AIRCRAFT 69
G. BRITTEN, J. BALLMANN: NUMERICAL EXPERIMENTS ABOUT THE UNIQUENESS OF
AEROELASTIC SOLUTIONS OFELASTIC WINGS IN TRANSONIC FLOW 77
O. BRODERSEN, E. MONSEN, A. RONZHETMER, R. RUDNIK, C.-C. ROSSOW: COM
PUTATION OF AERODYNAMIC COEFFICIENTS FOR THE DLR F-6 CONFIGURATION USING
MEGAFLOW.. 85
U. BURGGRAF,M. KUNTZ, B. SCHONING: IMPLEMENTATION OFTHE CHIMERAMETHOD IN
THE UNSTRUCTURED DLR FINITE VOLUME CODE TAU 93
D. DELIMAR, M. SWOBODA,M. LOTZERICH: NUMERICAL ANALYSES OFAN UNSTEADY
FLOW FIELD IN A COMPRESSOR CASCADE WITHPERIODICALLYCHANGING INFLOW
CONDITIONS 101
G. DIETZ, ST MAHLMANN, ST, HEIN: ENTROPY-LAYER INSTABILITIES IN PLANE
SUPERSONIC FLOW 108
E. ELSHOLZ, H. STEINMEYER, D. JOHN: NAVIER-STOKES SOLUTIONS ON
WING-BODY-TAIL CONFIGURATIONS AND VISCOUS MESH ADAPTATION TECHNIQUE 116
R.H. ENGLER, CHR. KLEIN, P. MAY: PRESSURE SENSITIVE PAINT APPLICATION IN
LOW-SPEED FLOWS 124
IMAGE 3
CONTENTS (CONTINUED)
PAGE
P. ERB, B. EWALD, M. ROTH, C. TROPEA: *IN-SITU CALIBRATION PROCEDURE
FOR SURFACE-HOTFILM-SENSORS BASED ON A STAGNATIONPOINT FLOW 130
A. FEZER, M. KLOKER: TRANSITIONPROCESSES IN MACH 6.8 BOUNDARY LAYERS AT
VARYING TEMPERATURE CONDITIONS INVESTIGATED BY SPATIAL DIRECTNUMERICAL
SIMULATION 138
S.D. FONOV, R.H. ENGLER, CHR. KLEIN, S.V. MTHATLOV, V.E. MOSHAROV, V.P.
KULESH, V.N. RADCHENKO, F. SCHATRER: INVESTIGATIONS OFTHE PRESSURE
FIELDS ON THE OSCILLATING WINGS BY PRESSURE SENSITIVE PAINT 146
M.FRANKE, T. RUNG, E. ELSHOLZ, P. AUMANN, F. THIELE: NUMERICAL SIMU
LATION OFTHREE-DIMENSIONAL TRANSONIC FLOWS USING ADVANCED
TURBULENCE-TRANSPORTMODELS ... 154
W. FRITZ: NUMERICAL SIMULATION OFUNSTEADY VORTICAL FLOW ABOUT DELTA
WINGS OSCILLATING AT HIGH INCIDENCE 162
O. FROMMANN, D.FORBRICH: AERODYNAMIC OPTIMIZATION OF AIRPLANE WINGS
USING ANALOGY METHODS 170
TH. GERHOLD, J.EVANS: EFFICIENT COMPUTATION OF 3D-FLOWS FOR COMPLEX
CONFIGURATIONS WITH THE DLR-TAU CODE USING AUTOMATIC ADAPTATION 178
P. GIESE, R. HEINRICH, R. RADESPIEL: NUMERICAL PREDICTION OFDYNAMIC
DERIVATIVES FOR LIFTING BODIES WITH A NAVIER-STOKES SOLVER 186
C. GMELIN, U. RIST, S. WAGNER: INVESTIGATIONS OFACTIVE CONTROL OFWAVE
PACKETS AND COMPARABLE DISTURBANCES IN A BLASIUS BOUNDARY LAYER BY DNS
194
W. HAASE, E.H. HTRSCHEL, J. KRAMMER, H. RIEGER: MULTIDISCIPLINARY
AERODYNAMIC/STRUCTURE DYNAMICS HIGH-PERFORMANCE SIMULATION AND
OPTIMIZATION 202
P. R. HAKENESCH: YAW CONTROL USING ASYMMETRIC FOREBODY STRAKES AT HIGH
ANGLES OF ATTACK 210
H. HANSEN, I. SZABO: INVESTIGATION OF STALL CHARACTERISTICS OFAN A3XX
RELEVANT AIRFOIL UP TO HIGH REYNOLDS NUMBERS INTHE TECHNOLOGY PROGRAM
HAK 2 218
R. HEINRICH, N. KALITZIN: NUMERICAL SIMULATION OFTHREE-DIMENSIONAL FLOWS
USING THE CHIMERA-TECHNIQUE 226
R. HENKE: FIRST RESULTS FROM THE *A 320 HLF FIN PROGRAMME 234
T.J. HOTTL, R.FREEDRICH: FULLY DEVELOPED TURBULENT FLOW IN CONDUITS WITH
CIRCULAR CROSS SECTION 242
J. VANKEUK, J. BALLMANN: NUMERICAL SIMULATIONOF LAMINAR SYMMETRIC COMER
FLOWS IN THE HYPERSONIC REGIME 250
IMAGE 4
CONTENTS (CONTINUED)
PAGE
T. KRIBLER: A CONCEPTUAL DESIGN METHODOLOGY FOR THE ESTIMATION OFTHE
LOCAL SHOCK LOCATIONSON OPTIMIZED TRANSONIC WINGS 258
N. LANG: INVESTIGATION OFTHEFLOW TRACKING CAPABILITIES OFTRACER
PARTICLES FOR THE APPLICATIONOFPRV TO SUPERSONIC FLOW FIELDS 266
B. LEHMANN, J. MANTE: TURBULENCE BEHAVIOUR OF SWIRLED DUAL-STREAM NOZZLE
FLOWS WITHOUT AND WITH COMBUSTION 274
J.A. LIESER, I. WALLBRUCH: CFD CALCULATIONS OFISOLATED JET ENGINES WITH
EMPHASIS ONJET MIXING 282
T. LOESER, K. DE GROOT, K.H. HORSTMANN: DESIGN OF AN INTEGRAL PROBE FOR
TEMPERATURE AND FLOW VECTOR MEASUREMENTS 291
M. MANHART: USING ZONAL GRIDS FORDIRECTNUMERICAL SIMULATION OFTURBULENT
BOUNDARY LAYERS WITH PRESSURE GRADIENTS 299
U. MAUCHER, U. RIST, S. WAGNER: TRANSITIONAL STRUCTURES IN A LAMINAR
SEPARATION BUBBLE 307
J. MERTENS: SOME IMPORTANT RESULTS OFTHE TECHNOLOGYPROGRAMME RAWID 315
R. MESSING, M. KLOKER, S. WAGNER: DIRECTNUMERICAL SIMULATION OFSUCTION
THROUGH DISCRETE HOLES IN A THREE-DIMENSIONALBOUNDARY LAYER 323
J. MULLER, D. HUMMEL: AN ANALYSIS OFVORTEX BREAKDOWN PREDICTED BY A
TIME-ACCURATE EULER CODE 331
P. NIEDERDRENK, O. BRODERSEN: CONTROLLED ELLIPTIC GRID GENERATION 339
D. RECKZEH: CFD-METHODS FOR THE DESIGN PROCESS
OFHIGH-LIFT-CONFIGURATIONS 347
C. ROSSOW: A SIMPLE FLUX SPLITTINGSCHEME FOR COMPRESSIBLE FLOWS 355
R. RUDNIK, A. RONZHEMER, J. RADDATZ: NUMERICAL FLOW SIMULATION FOR A
WING/FUSELAGE TRANSPORT AIRCRAFT CONFIGURATION WITH DEPLOYED HIGH-LIFT
SYSTEM 363
H. SANAKNAKI, J. BALLMANN: A NUMERICAL SIMULATION OFA 2D- VISCOUS
HYPERSONIC FLOW USING THE TIME-MARCHING METHODOFCHARACTERISTICS 371
S. SCHABER, H.E.FIEDLER: HOT WIRE MEASUREMENTS OF THE SUCTION
VELOCITYAND ITS DISTRIBUTION ON THE ELFIN U-WING MODEL WITH HYBRID
LAMINAR FLOW TECHNOLOGY 379
D. SCHIMKE, U.T.P. ARNOLD,W. GEMLER, R. KUBE, W.R. SPLETTSTOSSER: ACTIVE
ROTOR CONTROL BY SERVO-FLAP AND BLADE ROOT CONTROL: RECENT RESULTS FROM
FLIGHT TEST AND WINDTUNNEL 386
IMAGE 5
CONTENTS (CONTINUED)
PAGE
G. SCHRAUF, W. SCHRODER: COMPARISON OFN-FACTOR STRATEGIES USING WIND
TUNNEL EXPERIMENTS AND FLIGHTTESTS 394
N. SCHRODER, W. LOU, J. HOURMOUZIADIS: COMBINED TEST FACILITY FOR
THREE-DIMENSIONALMIXING LAYER AND UNSTEADY BOUNDARY LAYER RESEARCH 402
W. SCHRODER, G. SCHRAUF:DATAPREPARATION FOR THE STABILITY ANALYSIS OFTHE
ELFIN IIHLF WING MEASUREMENTS IN SIMA WIND TUNNEL 410
A. SCHUBERT, T. CORATEKIN, J. BALLMANN: NUMERICAL INVESTIGATIONOF
BOUNDARY LAYER SEPARATION CAUSED BY TURBULENT SHOCK/BOUNDARY LAYER
INTERACTION 418
D. SCHWAMBORN, T. GERHOLD, V. HANNEMANN: ON THE VALIDATION OFTHE
DLR-TAUCODE 426
W. SEND, R. VOB: EFFECTS OFA CONTOUR BUMP ON THE UNSTEADY TRANSONIC
AERODYNAMIC FORCES OFTHE AMP WING 434
R. SEUBERT: VALIDATION OFTHE PRELIMINARY AIRCRAFT DESIGN AND
OPTIMIZATION PROGRAM FOR SUPERSONIC COMMERCIAL TRANSPORT AIRCRAFT
PRADO-SUP 442
HA. SELLER, H.H. FERNHOLZ: ACTIVE SEPARATION CONTROL ON AN AIRFOIL BY A
PERIODIC CROSS-FLOW 450
C. STEMMER, J. SUTTAN, M. KLOKER, W. NTTSCHE: POINT-SOURCE INDUCED
TRANSITION IN FREE FLIGHT 458
D. STROHMEYER: EXTENSION OFTHEPREDESIGN CODE PRADO FORTHE EVALUATION OFA
THREE SURFACE AIRCRAFT 466
M. SWOBODA, R. TEUSCH, V. GUMMER, L. FOTTNER, U. WENGER: EXPERIMENTAL
INVESTIGATION OFBOUNDARY LAYER TRANSITION IN COMPRESSOR CASCADES AT
UNSTEADY PERIODIC FLOW CONDITIONS 474
O. TRINKS, W.H.BECK: APPLICATION OFTHE ABSORPTION SPECTROSCOPY FOR TIME
RESOLVED HYPERSONIC FLOWFIELD MEASUREMENTS USING THE D2-TRANSITION
OFSEEDED ATOMICRUBIDIUM 482
B. URBAN, H. STETTER, N. VORTMEYER: AERODYNAMIC EXITATION OFTRANSONIC
TURBINE CASCADE: DESCRIPTION OFTHE EXPERIMENTAL METHOD 488
P. VOIGT, P. THEISEN: EXPERIMENTAL ANALYSIS OFUNSTEADY MIXING IN ANRQL
COMBUSTORSEGMENT AIMED FOR VALIDATION OF PDF MODELS IN THE TRUST CODE
496
C. WAGNER, U.CH. DALLMANN: A DIRECT NAVIER-STOKES SOLVER FORTURBULENT
FLOWS OVER ROUND STEPS 505
IMAGE 6
CONTENTS (CONTINUED)
PAGE P. WASSERMANN, M. KLOKER: DIRECT NUMERICAL SIMULATION OFTHE
DEVELOPMENT AND CONTROL OFBOUNDARY-LAYER CROSSFLOW VORTICES 513 C.
WEISHAUPL, E. KREISELMATER, G. HELLER, B. LASCHKA: EULER CALCULATIONS
FOR THE FLOW AROUND A DELTA WING DURING FLAP OSCILLATIONS 521 W. WURZ,
S. HERR, S. WAGNER, Y.S. KACHANOV: EXPERIMENTAL INVESTIGATION ON 3D
ACOUSTIC RECEPTIVITYOFA LAMINAR BOUNDARY LAYER IN THE PRESENCE OF
SURFACENON-UNIFORMITIES 529
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| genre | (DE-588)1071861417 Konferenzschrift 1998 Berlin gnd-content |
| genre_facet | Konferenzschrift 1998 Berlin |
| id | DE-604.BV013141658 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T18:39:45Z |
| institution | BVB |
| isbn | 3528031220 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-008953234 |
| oclc_num | 43514225 |
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| owner_facet | DE-703 DE-210 DE-634 |
| physical | 536 S. graph. Darst. |
| publishDate | 1999 |
| publishDateSearch | 1999 |
| publishDateSort | 1999 |
| publisher | Vieweg |
| record_format | marc |
| series | Notes on numerical fluid mechanics |
| series2 | Notes on numerical fluid mechanics |
| spelling | New results in numerical and experimental fluid mechanics II contributions to the 11th AG STAB DGLR Symposium, Berlin, Germany, 1998 ed. by Wolfgang Nitsche ... Braunschweig Vieweg 1999 536 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Notes on numerical fluid mechanics 72 Aérodynamique - Congrès ram Aerodynamics Airplanes Design and construction Fluid dynamics Turbulence Congresses Strömungsmechanik (DE-588)4077970-1 gnd rswk-swf Flugzeugaerodynamik (DE-588)4135410-2 gnd rswk-swf Numerisches Verfahren (DE-588)4128130-5 gnd rswk-swf (DE-588)1071861417 Konferenzschrift 1998 Berlin gnd-content Flugzeugaerodynamik (DE-588)4135410-2 s DE-604 Strömungsmechanik (DE-588)4077970-1 s Numerisches Verfahren (DE-588)4128130-5 s Nitsche, Wolfgang Sonstige oth Notes on numerical fluid mechanics 72 (DE-604)BV000898664 72 GBV Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=008953234&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | New results in numerical and experimental fluid mechanics II contributions to the 11th AG STAB DGLR Symposium, Berlin, Germany, 1998 Notes on numerical fluid mechanics Aérodynamique - Congrès ram Aerodynamics Airplanes Design and construction Fluid dynamics Turbulence Congresses Strömungsmechanik (DE-588)4077970-1 gnd Flugzeugaerodynamik (DE-588)4135410-2 gnd Numerisches Verfahren (DE-588)4128130-5 gnd |
| subject_GND | (DE-588)4077970-1 (DE-588)4135410-2 (DE-588)4128130-5 (DE-588)1071861417 |
| title | New results in numerical and experimental fluid mechanics II contributions to the 11th AG STAB DGLR Symposium, Berlin, Germany, 1998 |
| title_auth | New results in numerical and experimental fluid mechanics II contributions to the 11th AG STAB DGLR Symposium, Berlin, Germany, 1998 |
| title_exact_search | New results in numerical and experimental fluid mechanics II contributions to the 11th AG STAB DGLR Symposium, Berlin, Germany, 1998 |
| title_full | New results in numerical and experimental fluid mechanics II contributions to the 11th AG STAB DGLR Symposium, Berlin, Germany, 1998 ed. by Wolfgang Nitsche ... |
| title_fullStr | New results in numerical and experimental fluid mechanics II contributions to the 11th AG STAB DGLR Symposium, Berlin, Germany, 1998 ed. by Wolfgang Nitsche ... |
| title_full_unstemmed | New results in numerical and experimental fluid mechanics II contributions to the 11th AG STAB DGLR Symposium, Berlin, Germany, 1998 ed. by Wolfgang Nitsche ... |
| title_short | New results in numerical and experimental fluid mechanics II |
| title_sort | new results in numerical and experimental fluid mechanics ii contributions to the 11th ag stab dglr symposium berlin germany 1998 |
| title_sub | contributions to the 11th AG STAB DGLR Symposium, Berlin, Germany, 1998 |
| topic | Aérodynamique - Congrès ram Aerodynamics Airplanes Design and construction Fluid dynamics Turbulence Congresses Strömungsmechanik (DE-588)4077970-1 gnd Flugzeugaerodynamik (DE-588)4135410-2 gnd Numerisches Verfahren (DE-588)4128130-5 gnd |
| topic_facet | Aérodynamique - Congrès Aerodynamics Airplanes Design and construction Fluid dynamics Turbulence Congresses Strömungsmechanik Flugzeugaerodynamik Numerisches Verfahren Konferenzschrift 1998 Berlin |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=008953234&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| volume_link | (DE-604)BV000898664 |
| work_keys_str_mv | AT nitschewolfgang newresultsinnumericalandexperimentalfluidmechanicsiicontributionstothe11thagstabdglrsymposiumberlingermany1998 |