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Volumn , Issue , 1996, Pages

Experiments on the active control of inlet noise from a turbofan jet engine using multiple circumferential control arrays

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELD MEASUREMENT; ACOUSTIC FIELDS; ACOUSTICS; AEROACOUSTICS; CONTROL SYSTEMS; DUCTS; ENGINES; TURBOFAN ENGINES;

EID: 0141869721     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1792     Document Type: Conference Paper
Times cited : (17)

References (20)
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  • 4
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    • Active Control of Fan Noise from a Turbofan Engine
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    • Burdisso, R.A.1    Thomas, R.H.2    Fuller, D.3    O’Brien, W.F.4
  • 5
  • 6
    • 0012856879 scopus 로고
    • Experiments on the active control of a turbofan inlet noise using compact, lightweight inlet control and error transducers
    • Munich, Germany
    • Burdisso, R. A., Fuller, C. R., and Smith, J. P., “Experiments on the active control of a turbofan inlet noise using compact, lightweight inlet control and error transducers,” First Joint CEAS/AIAA Aeroacoustic Conference, Munich, Germany, vol. 1, pp 177-185, June 1995.
    • (1995) First Joint CEAS/AIAA Aeroacoustic Conference , vol.1 , pp. 177-185
    • Burdisso, R.A.1    Fuller, C.R.2    Smith, J.P.3
  • 7
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    • Active control of fan-generated tone noise
    • Munich, Germany
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    • Gerhold, C.H.1
  • 8
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    • Application of active Helmholz resonator technology to plane wave duct acoustics
    • Munich, Germany, June
    • Walker, B. E., and Hersh, A. S., “Application of active Helmholz resonator technology to plane wave duct acoustics,” First Joint CEAS/AIAA Aeroacoustic Conference, Munich, Germany, vol. 1,pp 1115-1120, June 1995.
    • (1995) First Joint CEAS/AIAA Aeroacoustic Conference , vol.1 , pp. 1115-1120
    • Walker, B.E.1    Hersh, A.S.2
  • 9
    • 84977104242 scopus 로고
    • Active control of turbomachine discrete frequency noise utilizing oscillating flaps and pistons
    • Munich, Germany, June
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    • (1995) First Joint CEAS/AIAA Aeroacoustic Conference , vol.1 , pp. 195-204
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  • 11
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    • Acoustic Mode Measurements in the Inlet of a Turbofan Engine
    • Joppa, P. D., “Acoustic Mode Measurements in the Inlet of a Turbofan Engine,” Journal of Aircraft, Vol. 24, no. 9, Sept. 1987, p. 587-593.
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    • Joppa, P.D.1
  • 12
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    • Unsteady Fan Blade Pressure and Acoustic Radiation From a JT15D-1 Turbofan Engine at Simulated Forward Speed
    • January 12-15
    • Preisser, J. S., Schoenster, J. A., Golub, R. A., and Home, C., “Unsteady Fan Blade Pressure and Acoustic Radiation From a JT15D-1 Turbofan Engine at Simulated Forward Speed,” AIAA Paper 81-0096 presented at the 19th Aerospace Sciences Meeting, January 12-15, 1981.
    • (1981) 19Th Aerospace Sciences Meeting
    • Preisser, J.S.1    Schoenster, J.A.2    Golub, R.A.3    Home, C.4
  • 13
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    • Homyak, L., McArdle, J. G., and Heidelberg, L. J., “A Compact Inflow Control Device for SimulatingjaightEanNoise” AJAA J?aper-noJ83- 0680 presented at the AIAA 8”1 Aeroacoustic Conference, April 11-13, 1983.
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  • 14
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    • Analysis of Radiation Patterns of Interaction Tones Generated by Inlet Rods in the JT15D Engine
    • AIAA Paper no. 79-0581, March 12-14
    • Heidmann, M. F, Saule, A. V., and McArdle, J. G., “Analysis of Radiation Patterns of Interaction Tones Generated by Inlet Rods in the JT15D Engine,” AIAA Paper no. 79-0581, presented at the AIAA 5th Aeroacoustics Conference, March 12-14, 1979.
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    • Heidmann, M.F.1    Saule, A.V.2    McArdle, J.G.3
  • 16
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    • An Analytical Study of Active Control of Narrow-Band Turbofan Inlet Noise
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    • Burdisso, R.A., Fuller, C. R. and Glegg, S.A.L., “An Analytical Study of Active Control of Narrow-Band Turbofan Inlet Noise,” 16th AIAA Aeroacoustics Conference, Munich, Germany, 12- 15 June, 1995.
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  • 17
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  • 20
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.