The Resource Unsteady aerodynamics, aeroacoustics and aeroelasticity of turbomachines, edited by Kenneth C. Hall, Robert E. Kielb and Jeffrey P. Thomas, (electronic resource)

Unsteady aerodynamics, aeroacoustics and aeroelasticity of turbomachines, edited by Kenneth C. Hall, Robert E. Kielb and Jeffrey P. Thomas, (electronic resource)

Label
Unsteady aerodynamics, aeroacoustics and aeroelasticity of turbomachines
Title
Unsteady aerodynamics, aeroacoustics and aeroelasticity of turbomachines
Statement of responsibility
edited by Kenneth C. Hall, Robert E. Kielb and Jeffrey P. Thomas
Creator
Contributor
Subject
Genre
Language
eng
Summary
This textbook is a collection of technical papers that were presented at the 10th International Symposium on Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines held September 8-11, 2003 at Duke University in Durham, North Carolina. The papers represent the latest in state of the art research in the areas of aeroacoustics, aerothermodynamics, computational methods, experimental testing related to flow instabilities, flutter, forced response, multistage, and rotor-stator effects for turbomachinery
Cataloging source
COO
Dewey number
621.406
Illustrations
illustrations
Index
no index present
LC call number
TJ267
LC item number
.I57 2003
Literary form
non fiction
http://bibfra.me/vocab/lite/meetingDate
2003
http://bibfra.me/vocab/lite/meetingName
International Symposium on Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines
Nature of contents
  • dictionaries
  • bibliography
  • handbooks
http://library.link/vocab/relatedWorkOrContributorName
  • Hall, Kenneth C
  • Kielb, Robert E
  • Thomas, Jeffrey P
http://library.link/vocab/subjectName
  • Turbomachines
  • Unsteady flow (Aerodynamics)
  • Aeroelasticity
  • TECHNOLOGY & ENGINEERING
  • Ingénierie
  • Aeroelasticity
  • Turbomachines
  • Unsteady flow (Aerodynamics)
Label
Unsteady aerodynamics, aeroacoustics and aeroelasticity of turbomachines, edited by Kenneth C. Hall, Robert E. Kielb and Jeffrey P. Thomas, (electronic resource)
Link
http://dx.doi.org/10.1007/1-4020-4605-7
Instantiates
Publication
Note
International conference proceedings
Bibliography note
Includes bibliographical references
Carrier category
online resource
Carrier category code
  • cr
Carrier MARC source
rdacarrier
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Contents
Flutter -- FLUTTER BOUNDARIES FOR PAIRS OF LOW PRESSURE TURBINE BLADES -- INFLUENCE OF A VIBRATION AMPLITUDE DISTRIBUTION ON THE AERODYNAMIC STABILITY OF A LOW-PRESSURE TURBINE SECTORED VANE -- A METHOD TO ASSESS FLUTTER STABILITY OF COMPLEX MODES -- FLUTTER DESIGN OF LOWPRESSURE TURBINE BLADES WITH CYCLIC SYMMETRIC MODES -- EXPERIMENTAL AND NUMERICAL INVESTIGATION OF 2D PALISADE FLUTTER FOR THE HARMONIC OSCILLATIONS -- POSSIBILITY OF ACTIVE CASCADE FLUTTER CONTROL WITH SMART STRUCTURE IN TRANSONIC FLOWCONDITION -- EXPERIMENTAL FLUTTER INVESTIGATIONS OF AN ANNULAR COMPRESSOR CASCADE: INFLUENCE OF REDUCED FREQUENCY ON STABILITY -- FORCED RESPONSE -- UNSTEADY GUST RESPONSE IN THE FREQUENCY DOMAIN -- AXIAL TURBINE BLADE VIBRATIONS INDUCED BY THE STATOR FLOW -- MISTUNING AND COUPLING EFFECTS IN TURBOMACHINERY BLADINGS -- EVALUATION OF THE PRINCIPLE OF AERODYNAMIC SUPERPOSITION IN FORCED RESPONSE CALCULATIONS -- COMPARISON OF MODELS TO PREDICT LOW ENGINE ORDER EXCITATION IN A HIGH PRESSURE TURBINE STAGE -- EXPERIMENTAL REDUCTION OF TRANSONIC FAN FORCED RESPONSE BY IGV FLOW CONTROL -- MULTISTAGE EFFECTS -- UNSTEADY AERODYNAMIC WORK ON OSCILLATING ANNULAR CASCADES IN COUNTER ROTATION -- STRUCTURE OF UNSTEADY VORTICAL WAKES BEHIND BLADES OF MUTUAL-MOVING ROWS OF AN AXIAL TURBOMACHINE -- THE EFFECT OF MACH NUMBER ON LP TURBINEWAKE-BLADE INTERACTION -- MULTISTAGE COUPLING FOR UNSTEADY FLOWSIN TURBOMACHINERY -- AEROACOUSTICS -- PASSIVE NOISE CONTROL BY VANE LEAN AND SWEEP -- INTERACTION OF ACOUSTIC AND VORTICAL DISTURBANCES WITH AN ANNULAR CASCADE IN A SWIRLING FLOW -- INFLUENCE OF MUTUAL CIRCUMFERENTIAL SHIFT OF STATORS ON THE NOISE GENERATED BY SYSTEM OF ROWS STATOR-ROTOR-STATOR OF THE AXIAL COMPRESSOR -- A FREQUENCY-DOMAIN SOLVER FOR THE NON-LINEAR PROPAGATION AND RADIATION OF FAN NOISE -- FLOW INSTABILITIES -- ANALYSIS OF UNSTEADY CASING PRESSURE MEASUREMENTS DURING SURGE AND ROTATING STALL -- CORE-COMPRESSOR ROTATING STALL SIMULATION WITH A MULTI-BLADEROW MODEL -- PARAMETRIC STUDYOF SURFACE ROUGHNESS ANDWAKE UNSTEADINESS ON A FLAT PLATE WITH LARGE PRESSURE GRADIENT -- BYPASS FLOW PATTERN CHANGES AT TURBO-RAM TRANSIENT OPERATION OF A COMBINED CYCLE ENGINE -- EXPERIMENTAL INVESTIGATION OFWAKE-INDUCED TRANSITION IN A HIGHLY LOADED LINEAR COMPRESSOR CASCADE -- EXPERIMENTAL OFF-DESIGN INVESTIGATION OF UNSTEADY SECONDARY FLOWPHENOMENA IN A THREE-STAGE AXIAL COMPRESSOR AT 100% NOMINAL SPEED -- ANALYSES OF URANS AND LES CAPABILITIES TO PREDICT VORTEX SHEDDING FOR RODS AND TURBINES -- COMPUTATIONAL TECHNIQUES -- FREQUENCY AND TIME DOMAIN FLUID-STRUCTURE COUPLING METHODS FOR TURBOMACHINERIES -- STUDY OF SHOCK MOVEMENT AND UNSTEADY PRESSURE ON 2D GENERIC MODEL -- NUMERICAL UNSTEADY AERODYNAMICS FOR TURBOMACHINERY AEROELASTICITY -- DEVELOPMENT OF AN EFFICIENT AND ROBUST LINEARISED NAVIER-STOKES FLOW SOLVER -- OPTIMIZED DUAL-TIME STEPPING TECHNIQUE FOR TIME-ACCURATE NAVIER-STOKES CALCULATIONS -- EXPERIMENTAL UNSTEADY AERODYNAMICS -- EXPERIMENTAL AND NUMERICAL STUDY OF NONLINEAR INTERACTIONS IN TWO-DIMENSIONAL TRANSONIC NOZZLE FLOW -- INTERACTION BETWEEN SHOCKWAVES AND CASCADED BLADES -- MEASURED AND CALCULATED UNSTEADY PRESSURE FIELD IN A VANELESS DIFFUSER OF A CENTRIFUGAL COMPRESSOR -- DPIV MEASUREMENTS OF THE FLOW FIELD BETWEEN A TRANSONIC ROTOR AND AN UPSTREAM STATOR -- UNSTEADY PRESSURE MEASUREMENT WITH CORRECTION ON TUBING DISTORTION -- AEROTHERMODYNAMICS -- UNSTEADY 3D NAVIER-STOKES CALCULATION OF A FILM-COOLED TURBINE STAGE WITH DISCRETE COOLING HOLE -- ANALYSIS OF UNSTEADY AEROTHERMODYNAMIC EFFECTS IN A TURBINE-COMBUSTOR -- ROTOR STATOR INTERACTION -- STATOR-ROTOR AEROELASTIC INTERACTION FOR THE TURBINE LAST STAGE IN 3D TRANSONIC FLOW -- EFFECTS OF STATOR CLOCKINGINSYSTEMOF ROWS STATOR-ROTOR-STATOROF THE SUBSONICAXIAL COMPRESSOR -- ROTOR-STATOR INTERACTION IN A HIGHLY-LOADED, SINGLE-STAGE, LOW-SPEED AXIAL COMPRESSOR:UNSTEADY MEASUREMENTS IN THE ROTOR RELATIVE FRAME -- TWO-STAGE TURBINE EXPERIMENTAL INVESTIGATIONS OF UNSTEADY STATOR-TO-STATOR INTERACTION
Dimensions
unknown
Extent
1 online resource (x, 626 pages)
Form of item
online
Isbn
9781402046056
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations
Specific material designation
remote
Stock number
978-1-4020-4267-6
System control number
  • (OCoLC)77567540
  • (OCoLC)ocm77567540
Label
Unsteady aerodynamics, aeroacoustics and aeroelasticity of turbomachines, edited by Kenneth C. Hall, Robert E. Kielb and Jeffrey P. Thomas, (electronic resource)
Link
http://dx.doi.org/10.1007/1-4020-4605-7
Publication
Note
International conference proceedings
Bibliography note
Includes bibliographical references
Carrier category
online resource
Carrier category code
  • cr
Carrier MARC source
rdacarrier
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Contents
Flutter -- FLUTTER BOUNDARIES FOR PAIRS OF LOW PRESSURE TURBINE BLADES -- INFLUENCE OF A VIBRATION AMPLITUDE DISTRIBUTION ON THE AERODYNAMIC STABILITY OF A LOW-PRESSURE TURBINE SECTORED VANE -- A METHOD TO ASSESS FLUTTER STABILITY OF COMPLEX MODES -- FLUTTER DESIGN OF LOWPRESSURE TURBINE BLADES WITH CYCLIC SYMMETRIC MODES -- EXPERIMENTAL AND NUMERICAL INVESTIGATION OF 2D PALISADE FLUTTER FOR THE HARMONIC OSCILLATIONS -- POSSIBILITY OF ACTIVE CASCADE FLUTTER CONTROL WITH SMART STRUCTURE IN TRANSONIC FLOWCONDITION -- EXPERIMENTAL FLUTTER INVESTIGATIONS OF AN ANNULAR COMPRESSOR CASCADE: INFLUENCE OF REDUCED FREQUENCY ON STABILITY -- FORCED RESPONSE -- UNSTEADY GUST RESPONSE IN THE FREQUENCY DOMAIN -- AXIAL TURBINE BLADE VIBRATIONS INDUCED BY THE STATOR FLOW -- MISTUNING AND COUPLING EFFECTS IN TURBOMACHINERY BLADINGS -- EVALUATION OF THE PRINCIPLE OF AERODYNAMIC SUPERPOSITION IN FORCED RESPONSE CALCULATIONS -- COMPARISON OF MODELS TO PREDICT LOW ENGINE ORDER EXCITATION IN A HIGH PRESSURE TURBINE STAGE -- EXPERIMENTAL REDUCTION OF TRANSONIC FAN FORCED RESPONSE BY IGV FLOW CONTROL -- MULTISTAGE EFFECTS -- UNSTEADY AERODYNAMIC WORK ON OSCILLATING ANNULAR CASCADES IN COUNTER ROTATION -- STRUCTURE OF UNSTEADY VORTICAL WAKES BEHIND BLADES OF MUTUAL-MOVING ROWS OF AN AXIAL TURBOMACHINE -- THE EFFECT OF MACH NUMBER ON LP TURBINEWAKE-BLADE INTERACTION -- MULTISTAGE COUPLING FOR UNSTEADY FLOWSIN TURBOMACHINERY -- AEROACOUSTICS -- PASSIVE NOISE CONTROL BY VANE LEAN AND SWEEP -- INTERACTION OF ACOUSTIC AND VORTICAL DISTURBANCES WITH AN ANNULAR CASCADE IN A SWIRLING FLOW -- INFLUENCE OF MUTUAL CIRCUMFERENTIAL SHIFT OF STATORS ON THE NOISE GENERATED BY SYSTEM OF ROWS STATOR-ROTOR-STATOR OF THE AXIAL COMPRESSOR -- A FREQUENCY-DOMAIN SOLVER FOR THE NON-LINEAR PROPAGATION AND RADIATION OF FAN NOISE -- FLOW INSTABILITIES -- ANALYSIS OF UNSTEADY CASING PRESSURE MEASUREMENTS DURING SURGE AND ROTATING STALL -- CORE-COMPRESSOR ROTATING STALL SIMULATION WITH A MULTI-BLADEROW MODEL -- PARAMETRIC STUDYOF SURFACE ROUGHNESS ANDWAKE UNSTEADINESS ON A FLAT PLATE WITH LARGE PRESSURE GRADIENT -- BYPASS FLOW PATTERN CHANGES AT TURBO-RAM TRANSIENT OPERATION OF A COMBINED CYCLE ENGINE -- EXPERIMENTAL INVESTIGATION OFWAKE-INDUCED TRANSITION IN A HIGHLY LOADED LINEAR COMPRESSOR CASCADE -- EXPERIMENTAL OFF-DESIGN INVESTIGATION OF UNSTEADY SECONDARY FLOWPHENOMENA IN A THREE-STAGE AXIAL COMPRESSOR AT 100% NOMINAL SPEED -- ANALYSES OF URANS AND LES CAPABILITIES TO PREDICT VORTEX SHEDDING FOR RODS AND TURBINES -- COMPUTATIONAL TECHNIQUES -- FREQUENCY AND TIME DOMAIN FLUID-STRUCTURE COUPLING METHODS FOR TURBOMACHINERIES -- STUDY OF SHOCK MOVEMENT AND UNSTEADY PRESSURE ON 2D GENERIC MODEL -- NUMERICAL UNSTEADY AERODYNAMICS FOR TURBOMACHINERY AEROELASTICITY -- DEVELOPMENT OF AN EFFICIENT AND ROBUST LINEARISED NAVIER-STOKES FLOW SOLVER -- OPTIMIZED DUAL-TIME STEPPING TECHNIQUE FOR TIME-ACCURATE NAVIER-STOKES CALCULATIONS -- EXPERIMENTAL UNSTEADY AERODYNAMICS -- EXPERIMENTAL AND NUMERICAL STUDY OF NONLINEAR INTERACTIONS IN TWO-DIMENSIONAL TRANSONIC NOZZLE FLOW -- INTERACTION BETWEEN SHOCKWAVES AND CASCADED BLADES -- MEASURED AND CALCULATED UNSTEADY PRESSURE FIELD IN A VANELESS DIFFUSER OF A CENTRIFUGAL COMPRESSOR -- DPIV MEASUREMENTS OF THE FLOW FIELD BETWEEN A TRANSONIC ROTOR AND AN UPSTREAM STATOR -- UNSTEADY PRESSURE MEASUREMENT WITH CORRECTION ON TUBING DISTORTION -- AEROTHERMODYNAMICS -- UNSTEADY 3D NAVIER-STOKES CALCULATION OF A FILM-COOLED TURBINE STAGE WITH DISCRETE COOLING HOLE -- ANALYSIS OF UNSTEADY AEROTHERMODYNAMIC EFFECTS IN A TURBINE-COMBUSTOR -- ROTOR STATOR INTERACTION -- STATOR-ROTOR AEROELASTIC INTERACTION FOR THE TURBINE LAST STAGE IN 3D TRANSONIC FLOW -- EFFECTS OF STATOR CLOCKINGINSYSTEMOF ROWS STATOR-ROTOR-STATOROF THE SUBSONICAXIAL COMPRESSOR -- ROTOR-STATOR INTERACTION IN A HIGHLY-LOADED, SINGLE-STAGE, LOW-SPEED AXIAL COMPRESSOR:UNSTEADY MEASUREMENTS IN THE ROTOR RELATIVE FRAME -- TWO-STAGE TURBINE EXPERIMENTAL INVESTIGATIONS OF UNSTEADY STATOR-TO-STATOR INTERACTION
Dimensions
unknown
Extent
1 online resource (x, 626 pages)
Form of item
online
Isbn
9781402046056
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations
Specific material designation
remote
Stock number
978-1-4020-4267-6
System control number
  • (OCoLC)77567540
  • (OCoLC)ocm77567540

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