Suppression of self-sustained oscillations in a supersonic impinging jet

AIAA Journal

Volumn 39, Issue 12, 2001, Pages 2366-2373

  Elavarasan, R ^a,b   Krothapalli, A ^a,b   Venkatakrishnan, L ^a,b   Lourenco, L ^a,b  

^a FLORIDA A AND M UNIVERSITY   (United States)

^b FLORIDA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE PROPAGATION; AIR ENTRAINMENT; LIFT; OSCILLATIONS; SUPERSONIC FLOW; VELOCITY MEASUREMENT; VORTEX FLOW;

SUPERSONIC IMPRINGING JETS;

JETS;

EID: 0035665999     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1243     Document Type: Article

References (14)

1. Flow field and noise characteristics of a supersonic impinging jet
2. On the mechanism of choked jet noise
3. The sound-producing oscillations of round underexpanded jets impinging on normal plates
4. Acoustic feedback of a subsonic and supersonic free jet which impinges on an obstacle
5. Theoretical model of discrete tone generation by impinging jets
6. Mean and unsteady flowfield properties of supersonic impinging jets with lift plates
7. Some features of an edge tone flow field
8. Application of PIV to large-scale STOVL supersonic jet facility
9. Mesh-free, second-order accurate algorithm for PIV processing
10. True resolution PIV: A mesh-free second-order accurate algorithm
11. Observations on the boundary layer based on measured correlations with various improvements
12. Propagation velocity and space-time correlation of perturbations in turbulent channel flow