rdf-syntax-grammar
mods:
  schema location: http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
  title info:
    title: UNSTEADY AERODYNAMICS, AEROACOUSTICS AND AEROELASTICITY OF TURBOMACHINES
  name:
    name part: Hall, Kenneth C.
    role:
      role term: editor.
  name:
    name part: Kielb, Robert E.
    role:
      role term: editor.
  name:
    name part: Thomas, Jeffrey P.
    role:
      role term: editor.
  name:
    name part: SpringerLink (Online service)
  type of resource: text
  origin info:
    place:
      place term: ne
    date issued: 2006
    issuance: monographic
  language:
    language term: eng
  physical description:
    form: electronic
    form: electronic resource
    reformatting quality: access
    form: remote
    extent: XII, 626 p. online resource.
  abstract: 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.
  table of 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 -- PARAMET…
  note: edited by Kenneth C. Hall, Robert E. Kielb, Jeffrey P. Thomas.
  subject:
    topic: Engineering
  subject:
    topic: Mechanical engineering
  subject:
    topic: Machinery
  subject:
    topic: Automotive engineering
  subject:
    topic: Engineering
  subject:
    topic: Mechanical Engineering
  subject:
    topic: Automotive Engineering
  subject:
    topic: Engineering, general
  subject:
    topic: Machinery and Machine Elements
  classification: TJ1-1570
  classification: 621
  related item:
    title info:
      title: Springer eBooks
  identifier: 9781402046056
  identifier: http://dx.doi.org/10.1007/1-4020-4605-7
  record info:
    record creation date: 100301
    record change date: 20151204190154.0
    record identifier: 978-1-4020-4605-6