The effects of nozzle exit lip thickness on plume resonance

Journal of Sound and Vibration

Volumn 154, Issue 3, 1992, Pages 531-549

  Ponton, M K ^a   Seiner, J M ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0002942882     PISSN: 0022460X     EISSN: 10958568     Source Type: Journal    
DOI: 10.1016/0022-460X(92)90784-U     Document Type: Article

References (15)

1. On the mechanism of choked jet noise
2. Proposed relationship between broadband shock associated noise and screech tones
3. Tones from a choked axisymmetric jet, I: cell structure, eddy velocity and source locations; II: the self excited loop and mode of oscillation
4. The photographic evidence of the feedback loop of a two-dimensional screeching supersonic jet of air
5. Screech suppression in supersonic jets
6. The influence of nozzle asymmetry on supersonic jets
7. Acoustic properties associated with rectangular geometry supersonic nozzles
8. On spatially growing disturbances in an inviscid shear layer
9. Perturbed free shear layers
10. The radiation of sound by the instability waves of a compressible plane turbulent shear layer
11. Aeroacoustic research facilities at NASA Langley Research Center-description and operational characteristics
12. A short static-pressure probe design for supersonic flow
13. Advances in high speed jet aeroacoustics
14. The noise from shock waves in supersonic jets