Adaptive flow control of supersonic impinging jets

15th AIAA Computational Fluid Dynamics Conference

Volumn , Issue , 2001, Pages

  Shih, C ^a   Alvi, F S ^a   Lou, H ^a   Garg, G ^a   Krotbapalli, A ^a  

^a FLORIDA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894443597     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

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2. Alvi, F.S., Shih, C. and Krothapalli, A., Active Control Of The Feedback Loop in High-Speed Jets, AIAA Paper 2001-0373
3. Powell, A., The Sound-Producing Oscillations of Round Underexpanded Jets Impinging on Nonnal Plates, J. Acoust Soc. Am., 83 (2), 1988, 515-533.
4. Neuwerth, G.,Acoustic Feedback of a subsonic and Supersonic Free Jet which Impinges on an Obstacle, NASA TT F-15719,1974.
5. Tarn, C.K.W., and Ahuja, K.K., Theoretical model of discrete tone generation by impinging jets, J. Fluid Mech., Vol. 214,1990, pp 67-87.
6. Karamcheti, K., Bauer, A.B., Shields, W.L., Stegen, G.R., And Woolley, J.P., Some Features of an Edge Tone Flow Field, NASA SP 207, 1969,pp275-304.
7. Elavarasan, R., Krothapalli, A., Venkatakrishnan, L. and Lourenco, L., Suppression of selfsustained oscillations in a supersonic impinging jet. Submitted for publication in AIAA journal. Also see, Elavarasan R., Venkatakrishnan, LKrothapalli, A. and Lourenco, L., A PIV study of a supersonic impinging jet, Journal of Visualization, Vol. 2, No.3/4,213-222, 2000.
8. Glass, D.R., Effect of acoustic feedback on the spread and decay of supersonic jets, AIAA Journal Vol.6, No.6, 1968, pp1890-1897.
9. Poldervaart, L.J., Wijnands, A.P.J., vanMoll, L.H.A.M., and vanVoorthuisen, E.J., Modes of vibration, J. Fluid Mech, Vol. 78, 1976, pp.859-862.
10. Alvi, F S. and Iyer, K. G., Mean and Unsteady Flowfield Properties Of Supersonic Impinging Jets With Lift Plates, AIAA Paper 99-1829, presented at the 5th AIAA/CEAS Aeroacoustics Conference, May 1999.
11. Sheplak, M. and Spina, E.F., Control of highspeed impinging-jet resonance, AIAA Journal, Vol.32, No.8,1994, pp1583-1588.
12. Shih, C., AM, F. S., and Washington, D., Effects of Counterflow on the Aeroacoustic Properties of a Supersonic Jet, AIAA Journal of Aircraft, Vol. 36, No. 2, March/April 1999, pp. 451-457.
13. Samimy, M. Zaman, K. B. M.Q. and Reeder, M. F., Effect of Tabs on the Flow and Noise Field of an Axisymmetric Jets, AIAA Journal, Vol.31, No.4, 1993, pp. 609-619.
14. Krothapalli A., Strykowski P. J. and King C. J., Origin of Streamwise Vortices in Supersonic Jets, AIAA Journal, Vol. 36: No. 5,1998, pp. 869-872.
15. Krothapalli, A., Rajakuperan, E. Alvi, F. S. and Lourenco, L., Flow field and Noise Characteristics of a Supersonic Impinging Jet, Journal of Fluid Mechanics, Vol. 392, August 1999, pp. 155-181.
16. Phalnikar, K.A., Alvi, F.S., and Shih, C., Behavior of Free and Impinging Supersonic Microjets, AIAA Paper 2001-3047.
17. Ibrahim, M.K and Nakamura, Y., Effects of Rotating Tabs on Row and Acoustic Fields of Supersonic Jet, AIAA Journal, Vol. 39, No. 4, pp745-748,2001.