Advances in simulation of wing and nacelle stall: results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany
Gespeichert in:
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| Weitere Verfasser: | , , , |
| Format: | Elektronisch Tagungsbericht E-Book |
| Sprache: | English |
| Veröffentlicht: |
Cham
Springer International Publishing
[2016]
|
| Schriftenreihe: | Notes on numerical fluid mechanics and multidisciplinary design
volume 131 |
| Schlagworte: | |
| Online-Zugang: | BTU01 FAB01 FAW01 FHA01 FHI01 FHN01 FHR01 FKE01 FRO01 FWS01 FWS02 UBY01 Volltext Inhaltsverzeichnis Abstract |
| Beschreibung: | 1 Online Ressource (IX, 413 Seiten) |
| ISBN: | 9783319211275 |
| DOI: | 10.1007/978-3-319-21127-5 |
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Datensatz im Suchindex
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| adam_text | ADVANCES IN SIMULATION OF WING AND NACELLE STALL
/
: 2016
TABLE OF CONTENTS / INHALTSVERZEICHNIS
THE DELAY OF RANS-TO-LES TRANSITION IN HYBRID RANS-LES APPROACHES AND
SOME RECENTLY PROPOSED REMEDIES
COMPUTATIONS OF SEPARATED FLOWS WITH A HYBRID RANS/LES APPROACH
HYBRID RANS/LES STUDY OF THE DEVELOPMENT OF AN AIRFOIL-GENERATED VORTEX
INTERACTION OF THREE-DIMENSIONAL DISTURBANCES WITH THE FLOW AROUND A
TWO-ELEMENT HIGH-LIFT AIRFOIL
THE DISCONTINUOUS GALERKIN METHOD AS AN ENABLING TECHNOLOGY FOR DNS AND
LES OF INDUSTRIAL AERONAUTICAL APPLICATIONS
BODY FORCE MODELLING OF INTERNAL GEOMETRY FOR JET NOISE PREDICTION
NUMERICAL STUDIES OF TURBULENT FLOW INFLUENCE ON A TWO-ELEMENT AIRFOIL
CFD FOR PREDICTION OF FLOW SEPARATION FROM AIRCRAFT TAIL SURFACES
ZONAL RANS-LES COMPUTATION FOR NEAR-STALL-AIRFOIL FLOW
CRITERIA FOR CROSSWIND VARIATIONS DURING APPROACH AND TOUCHDOWN AT
AIRPORTS
DEVELOPMENT AND IMPROVEMENT OF TWO METHODS OF DIFFERENT COMPLEXITY TO
SIMULATE ATMOSPHERIC BOUNDARY LAYER TURBULENCE FOR AIRCRAFT DESIGN
STUDIES
SIMULATION OF INTERACTION OF AIRCRAFT WITH GUST AND RESOLVED
LES-SIMULATED ATMOSPHERIC TURBULENCE
A NEW METHOD TO GENERATE ANISOTROPIC SYNTHETIC TURBULENCE FOR LES
NUMERICAL SIMULATION OF THE TURBULENT FLOW AROUND A WING
INTEGRATION- AND INTAKE-INDUCED FLOW DISTORTIONS AND THEIR IMPACT ON
AERODYNAMIC FAN PERFORMANCE
FLOW INVESTIGATIONS IN A STALLING NACELLE INLET UNDER DISTURBED INFLOW
REALISTIC INLET DISTORTION PATTERNS INTERACTING WITH A TRANSONIC
COMPRESSOR STAGE
UNSTEADY CFD SIMULATION OF TRANSONIC AXIAL COMPRESSOR STAGES WITH
DISTORTED INFLOW
TRANSITIONAL SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS IN INTAKES AT
INCIDENCE.-ADVANCED DESIGN APPROACH FOR A HIGH-LIFT WIND TUNNEL MODEL
BASED ON FLIGHT TEST DATA
SIMULATION OF LONGITUDINAL VORTICES ON A HIGH-LIFTWING
IMPACT OF DIFFERENT UHBR-ENGINE POSITIONS ON THE AERODYNAMICS OF A
HIGH-LIFTWING
NUMERICAL INVESTIGATION OF THE INFLUENCE OF PRESSURE BELTS ON THE STALL
OF A TRANSPORT AIRCRAFT IN LANDING CONFIGURATION
NUMERICAL STUDIES OF ACTIVE FLOW CONTROL APPLIED AT THE ENGINE-WING
JUNCTION
DIESES SCHRIFTSTUECK WURDE MASCHINELL ERZEUGT.
ADVANCES IN SIMULATION OF WING AND NACELLE STALL
/
: 2016
ABSTRACT / INHALTSTEXT
THE BOOK REPORTS ON ADVANCED SOLUTIONS TO THE PROBLEM OF SIMULATING WING
AND NACELLE STALL, AS PRESENTED AND DISCUSSED BY INTERNATIONALLY
RECOGNIZED RESEARCHERS AT THE CLOSING SYMPOSIUM OF THE DFG RESEARCH UNIT
FOR 1066. RELIABLE SIMULATIONS OF FLOW SEPARATION ON AIRFOILS, WINGS AND
POWERED ENGINE NACELLES AT HIGH REYNOLDS NUMBERS REPRESENT GREAT
CHALLENGES IN DEFINING SUITABLE MATHEMATICAL MODELS, COMPUTING
NUMERICALLY ACCURATE SOLUTIONS AND PROVIDING COMPREHENSIVE EXPERIMENTAL
DATA FOR THE VALIDATION OF NUMERICAL SIMULATIONS. ADDITIONAL PROBLEMS
ARISE FROM THE NEED TO CONSIDER AIRFRAME-ENGINE INTERACTIONS AND
INHOMOGENEOUS ONSET FLOW CONDITIONS, AS REAL AIRCRAFT OPERATE IN
ATMOSPHERIC ENVIRONMENTS WITH OFTEN-LARGE DISTORTIONS. THE FINDINGS OF
FUNDAMENTAL AND APPLIED RESEARCH INTO THESE AND OTHER RELATED ISSUES ARE
REPORTED IN DETAIL IN THIS BOOK, WHICH TARGETS ALL READERS, ACADEMICS
AND PROFESSIONALS ALIKE, INTERESTED IN THE DEVELOPMENT OF ADVANCED
COMPUTATIONAL FLUID DYNAMICS MODELING FOR THE SIMULATION OF COMPLEX
AIRCRAFT FLOWS WITH FLOW SEPARATION
DIESES SCHRIFTSTUECK WURDE MASCHINELL ERZEUGT.
|
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| author2 | Radespiel, Rolf Niehuis, Reinhard 1955- Kroll, Norbert Behrends, Kathrin |
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| author_corporate | Closing Symposium of the DFG Research Unit FOR 1066 |
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| author_facet | Radespiel, Rolf Niehuis, Reinhard 1955- Kroll, Norbert Behrends, Kathrin Closing Symposium of the DFG Research Unit FOR 1066 |
| author_sort | Closing Symposium of the DFG Research Unit FOR 1066 |
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| genre | 1\p (DE-588)1071861417 Konferenzschrift 2014 Braunschweig gnd-content |
| genre_facet | Konferenzschrift 2014 Braunschweig |
| id | DE-604.BV043212010 |
| illustrated | Not Illustrated |
| indexdate | 2024-08-01T12:12:20Z |
| institution | BVB |
| institution_GND | (DE-588)1092568492 |
| isbn | 9783319211275 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-028635148 |
| oclc_num | 916052086 |
| open_access_boolean | |
| owner | DE-706 DE-1043 DE-Aug4 DE-573 DE-859 DE-863 DE-BY-FWS DE-92 DE-862 DE-BY-FWS DE-898 DE-BY-UBR DE-634 DE-1046 DE-861 |
| owner_facet | DE-706 DE-1043 DE-Aug4 DE-573 DE-859 DE-863 DE-BY-FWS DE-92 DE-862 DE-BY-FWS DE-898 DE-BY-UBR DE-634 DE-1046 DE-861 |
| physical | 1 Online Ressource (IX, 413 Seiten) |
| psigel | ZDB-2-ENG ZDB-2-ENG_2016 |
| publishDate | 2016 |
| publishDateSearch | 2016 |
| publishDateSort | 2016 |
| publisher | Springer International Publishing |
| record_format | marc |
| series2 | Notes on numerical fluid mechanics and multidisciplinary design |
| spellingShingle | Advances in simulation of wing and nacelle stall results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany Engineering Fluids Fluid mechanics Aerospace engineering Astronautics Engineering Fluid Dynamics Fluid- and Aerodynamics Aerospace Technology and Astronautics Ingenieurwissenschaften Flugzeugaerodynamik (DE-588)4135410-2 gnd Tragflügel (DE-588)4060582-6 gnd Grenzschichtablösung (DE-588)4136915-4 gnd Triebwerksgondel (DE-588)4427302-2 gnd |
| subject_GND | (DE-588)4135410-2 (DE-588)4060582-6 (DE-588)4136915-4 (DE-588)4427302-2 (DE-588)1071861417 |
| title | Advances in simulation of wing and nacelle stall results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany |
| title_auth | Advances in simulation of wing and nacelle stall results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany |
| title_exact_search | Advances in simulation of wing and nacelle stall results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany |
| title_full | Advances in simulation of wing and nacelle stall results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany Rolf Radespiel, Reinhard Niehuis, Norbert Kroll, Kathrin Behrends editors |
| title_fullStr | Advances in simulation of wing and nacelle stall results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany Rolf Radespiel, Reinhard Niehuis, Norbert Kroll, Kathrin Behrends editors |
| title_full_unstemmed | Advances in simulation of wing and nacelle stall results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany Rolf Radespiel, Reinhard Niehuis, Norbert Kroll, Kathrin Behrends editors |
| title_short | Advances in simulation of wing and nacelle stall |
| title_sort | advances in simulation of wing and nacelle stall results of the closing symposium of the dfg research unit for 1066 december 1 2 2014 braunschweig germany |
| title_sub | results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany |
| topic | Engineering Fluids Fluid mechanics Aerospace engineering Astronautics Engineering Fluid Dynamics Fluid- and Aerodynamics Aerospace Technology and Astronautics Ingenieurwissenschaften Flugzeugaerodynamik (DE-588)4135410-2 gnd Tragflügel (DE-588)4060582-6 gnd Grenzschichtablösung (DE-588)4136915-4 gnd Triebwerksgondel (DE-588)4427302-2 gnd |
| topic_facet | Engineering Fluids Fluid mechanics Aerospace engineering Astronautics Engineering Fluid Dynamics Fluid- and Aerodynamics Aerospace Technology and Astronautics Ingenieurwissenschaften Flugzeugaerodynamik Tragflügel Grenzschichtablösung Triebwerksgondel Konferenzschrift 2014 Braunschweig |
| url | https://doi.org/10.1007/978-3-319-21127-5 http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=028635148&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=028635148&sequence=000003&line_number=0002&func_code=DB_RECORDS&service_type=MEDIA |
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