Computational and experimental study of linear aerospike engine noise

AIAA Journal

Volumn 39, Issue 8, 2001, Pages 1485-1492

  Frendi, Abdelkader ^a   Nesman, Tomas E ^b   Wang, Ten See ^b  

^a UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

^b NASA MARSHALL SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; COMPUTATIONAL FLUID DYNAMICS; MATHEMATICAL MODELS; NOZZLES; THERMAL PLUMES; TURBULENCE;

AEROSPIKE ENGINE NOISE;

JET ENGINES;

EID: 0035422542     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1499     Document Type: Article

References (23)

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2. On sound generated aerodynamically: I. Turbulence as a source of sound
3. Quadrupole correlations governing the pattern of jet noise
4. On the strength distribution of noise sources along a jet
5. On spectra and directivity of jet noise
6. Hydrodynamics noise
7. Aeroacoustics
8. Aeroacoustics of turbulent shear flows
9. Supersonic jet noise
10. The noise from turbulence convected at high speed
11. Computation of supersonic jet mixing noise from an axisymmetric CD nozzle using (k-ε) turbulence model
12. Jet noise predictions using a (k-ε) turbulence model
13. Prediction of supersonic jet noise from a statistical acoustic model and a compressible turbulence closure
14. Jet mixing noise from fine-scale turbulence
15. An experimental investigation of the circumstances which determine whether the motion of water will be direct or sinuous and the law of resistance in parallel channels
16. The acoustic field of sources in shear flow with application to jet noise: Convective amplification
17. High frequency sound emission from moving point multipole sources embedded in arbitrary transversely sheared mean flows
18. Analysis of linear aerospike plume-induced X-33 base-heating environment