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Acoustic sources in a tripped flow past a resonator tube

Identifieur interne : 007034 ( PascalFrancis/Corpus ); précédent : 007033; suivant : 007035

Acoustic sources in a tripped flow past a resonator tube

Auteurs : M. C. Thompson ; K. Hourigan ; M. C. Welsh ; E. Brocher

Source :

RBID : Pascal:92-0427596

Descripteurs français

English descriptors

Abstract

A numerical model employing the vortex method is used to investigate the separated flow around a trip rod placed upstream of a resonator tube. The acoustic power generated by the flow is calculated using Howe's theory of aerodynamic sound.

Notice en format standard (ISO 2709)

Pour connaître la documentation sur le format Inist Standard.

pA  
A01 01  1    @0 0001-1452
A02 01      @0 AIAJAH
A03   1    @0 AIAA j.
A05       @2 30
A06       @2 6
A08 01  1  ENG  @1 Acoustic sources in a tripped flow past a resonator tube
A11 01  1    @1 THOMPSON (M. C.)
A11 02  1    @1 HOURIGAN (K.)
A11 03  1    @1 WELSH (M. C.)
A11 04  1    @1 BROCHER (E.)
A14 01      @1 Commonwealth sci. industrial res. organisation @2 Highett Victoria 3190 @3 AUS @Z 1 aut., 2 aut., 3 aut.
A14 02      @1 Univ. Aix-Marseille @2 13003 Marseille @3 FRA @Z 4 aut.
A20       @1 1484-1491
A21       @1 1992
A23 01      @0 ENG
A43 01      @1 INIST @2 214 @5 354000028615660060
A44       @0 0000
A45       @0 15 ref.
A47 01  1    @0 92-0427596
A60       @1 P
A61       @0 A
A64   1    @0 AIAA journal
A66 01      @0 USA
C01 01    ENG  @0 A numerical model employing the vortex method is used to investigate the separated flow around a trip rod placed upstream of a resonator tube. The acoustic power generated by the flow is calculated using Howe's theory of aerodynamic sound.
C02 01  X    @0 001B05A
C03 01  X  FRE  @0 Détachement tourbillonnaire
C03 01  X  ENG  @0 Vortex shedding
C03 01  X  SPA  @0 Desprendimiento vorticial
C03 02  X  FRE  @0 Tube résonance
C03 02  X  ENG  @0 Resonance tube
C03 02  X  SPA  @0 Tubo resonancia
C03 03  X  FRE  @0 Résonateur acoustique
C03 03  X  ENG  @0 Acoustic resonator
C03 03  X  SPA  @0 Resonador acústico
C03 04  X  FRE  @0 Ecoulement
C03 04  X  ENG  @0 Flow(fluid)
C03 04  X  GER  @0 Fluide Stroemung
C03 04  X  SPA  @0 Flujo
C03 05  X  FRE  @0 Visualisation
C03 05  X  ENG  @0 Visualization
C03 05  X  SPA  @0 Visualización
C03 06  X  FRE  @0 Etude expérimentale
C03 06  X  ENG  @0 Experimental study
C03 06  X  GER  @0 Experimentelle Untersuchung
C03 06  X  SPA  @0 Estudio experimental
C03 07  X  FRE  @0 Champ acoustique
C03 07  X  ENG  @0 Acoustic field
C03 07  X  GER  @0 Schallfeld
C03 07  X  SPA  @0 Campo acústico
C03 08  X  FRE  @0 Obstacle
C03 08  X  ENG  @0 Obstacle
C03 08  X  SPA  @0 Obstáculo
N21       @1 255

Format Inist (serveur)

NO : PASCAL 92-0427596 INIST
ET : Acoustic sources in a tripped flow past a resonator tube
AU : THOMPSON (M. C.); HOURIGAN (K.); WELSH (M. C.); BROCHER (E.)
AF : Commonwealth sci. industrial res. organisation/Highett Victoria 3190/Australie (1 aut., 2 aut., 3 aut.); Univ. Aix-Marseille/13003 Marseille/France (4 aut.)
DT : Publication en série; Niveau analytique
SO : AIAA journal; ISSN 0001-1452; Coden AIAJAH; Etats-Unis; Da. 1992; Vol. 30; No. 6; Pp. 1484-1491; Bibl. 15 ref.
LA : Anglais
EA : A numerical model employing the vortex method is used to investigate the separated flow around a trip rod placed upstream of a resonator tube. The acoustic power generated by the flow is calculated using Howe's theory of aerodynamic sound.
CC : 001B05A
FD : Détachement tourbillonnaire; Tube résonance; Résonateur acoustique; Ecoulement; Visualisation; Etude expérimentale; Champ acoustique; Obstacle
ED : Vortex shedding; Resonance tube; Acoustic resonator; Flow(fluid); Visualization; Experimental study; Acoustic field; Obstacle
GD : Fluide Stroemung; Experimentelle Untersuchung; Schallfeld
SD : Desprendimiento vorticial; Tubo resonancia; Resonador acústico; Flujo; Visualización; Estudio experimental; Campo acústico; Obstáculo
LO : INIST-214.354000028615660060
ID : 92-0427596

Links to Exploration step

Pascal:92-0427596

Le document en format XML

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