Experimental investigation on the influence of liner non-uniformities on prevailing modes (of acoustic propagation in turbofan engines)

2nd AIAA/CEAS Aeroacoustics Conference

Volumn , Issue , 1996, Pages

  Rademaker, Edward R ^a   Sarin, Sohan L ^b   Parente, Charles A ^c  

^a NATIONAL AEROSPACE LABORATORY NLR   (Netherlands)

^b AIRBUS DEFENCE AND SPACE   (Germany)

^c NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELDS; ACOUSTICS; AEROACOUSTICS; DUCTS; ENGINES; FLOW VELOCITY; MODULATION; TURBOFAN ENGINES;

ACOUSTIC ENERGY FLUXES; ACOUSTIC PROPAGATION; AXISYMMETRIC FLOW; CIRCUMFERENTIAL MODES; EXPERIMENTAL INVESTIGATIONS; EXPERIMENTAL PROGRAM; MODULATION EFFECTS; TRANSMITTED FIELD;

ACOUSTIC WAVE SCATTERING;

EID: 84977090658     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1682     Document Type: Conference Paper

References (2)

1. Sarin, S.L., Rademaker, E.R., In-flight Acoustic Mode Measurements in the Turbofan Engine Inlet of Fokker 100 Aircraft, AIAA-paper 93-4414
2. Zandbergen, T., Stator Vane Response due to the Impingement of the Wake of an Unloaded Rotor, AIAA paper 89-1125