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Volumn , Issue , 2002, Pages

Microjet control of supersonic impinging jets - control strategy and physical mechanisms

Author keywords

[No Author keywords available]

Indexed keywords


EID: 84894627628     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (1)

References (20)
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  • 2
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    • The sound -producing oscillations of round underexpanded jets impinging on normal plates
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  • 3
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    • Theoretical model of discrete tone generation by impinging jet
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    • Tam, C.K.W.1    Ahuja, K.K.2
  • 4
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    • Flow field and Noise Characteristics of a Supersonic Impinging Jet
    • Krothapalli A., Rajakuperan, E., Alvi, F.S. and Lourenco, L., 1999 "Flow field and Noise Characteristics of a Supersonic Impinging Jet," J. Fluid. Mech., Vol. 392, pp. 155-181.
    • (1999) J. Fluid. Mech , vol.392 , pp. 155-181
    • Krothapalli, A.1    Rajakuperan, E.2    Alvi, F.S.3    Lourenco, L.4
  • 5
    • 0000991011 scopus 로고
    • Control of an axisymmetric jet using vortex generators
    • Feb
    • Zaman K.B.M.Q., Reeder. M.F. and Samimy, M., 1994 "Control of an axisymmetric jet using vortex generators," Phys. Fluids. 6 (2) Feb.
    • (1994) Phys. Fluids , vol.6 , Issue.2
    • Zaman, K.B.M.Q.1    Reeder, M.F.2    Samimy, M.3
  • 6
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    • Supersonic jet noise reduction and mixing enhancement through nozzle trailing edge modifications
    • Samimy M., Kim, J.H., and Clancy, P.S., 1997 "Supersonic jet noise reduction and mixing enhancement through nozzle trailing edge modifications," AIAA Paper 97-1046.
    • (1997) AIAA Paper 97-1046
    • Samimy, M.1    Kim, J.H.2    Clancy, P.S.3
  • 9
    • 4244126015 scopus 로고
    • Effect of acoustic feedback on the spread and decay of supersonic jets
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    • (1968) AIAA Journal , vol.6 , Issue.6 , pp. 1890-1897
    • Glass, D.R.1
  • 14
    • 0000812840 scopus 로고    scopus 로고
    • Origin of Streamwise Vortices in Supersonic Jets
    • Krothapalli A., Strykowski, P.J. and King, C. J., 1998 "Origin of Streamwise Vortices in Supersonic Jets," AIAA Journal, Vol. 36, No. 5, pp. 869-872.
    • (1998) AIAA Journal , vol.36 , Issue.5 , pp. 869-872
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  • 15
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    • Flowfield Properties of Supersonic Impinging Jets With Active Control
    • 1st AIAA Flow Control Conference and Exhibit, June, St. Luis, MO
    • Lou H. Alvi, F.S., Shih, C., Choi, J., and Annaswamy, A., "Flowfield Properties of Supersonic Impinging Jets With Active Control," AIAA Paper 2002-2728, 1st AIAA Flow Control Conference and Exhibit, June, St. Luis, MO.
    • AIAA Paper 2002-2728
    • Lou, H.1    Alvi, F.S.2    Shih, C.3    Choi, J.4    Annaswamy, A.5
  • 16
    • 0027576518 scopus 로고
    • Effect of Tabs on the Flow and Noise Field of an Axisymmetric Jets
    • Samimy M., Zaman, K.B.M.Q. and Reeder, M.F., 1993 "Effect of Tabs on the Flow and Noise Field of an Axisymmetric Jets," AIAA Journal, Vol. 31, No. 4, pp.609-619.
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  • 17
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    • Effect of Rotating Tabs on Flow and Acoustic Fields of Supersonic Jet
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  • 18
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    • Mixing enhancement via nozzle trailing edge modifications in a high speed rectangular jet
    • Kim J.H. and Samimy, M., 1999 "Mixing enhancement via nozzle trailing edge modifications in a high speed rectangular jet," Phys. Fluids, Vol. 11, No. 9, pp.2731-2742.
    • (1999) Phys. Fluids , vol.11 , Issue.9 , pp. 2731-2742
    • Kim, J.H.1    Samimy, M.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.