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Volumn 129, Issue 1, 2007, Pages 184-191

Preliminary fan design for a silent aircraft

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; DESIGN; NOISE ABATEMENT; SUPERSONIC AERODYNAMICS; TURBOMACHINE BLADES;

EID: 34248353948     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2372779     Document Type: Article
Times cited : (17)

References (34)
  • 1
    • 0011508350 scopus 로고    scopus 로고
    • Air Travel - Greener by design: The Technology Challenge
    • Greener by Design
    • "Air Travel - Greener by design: The Technology Challenge," Greener by Design 2001.
    • (2001)
  • 2
    • 4344652744 scopus 로고    scopus 로고
    • Department for Transport, UK Government
    • "The Future of Air Transport," Department for Transport, UK Government 2003.
    • (2003) The Future of Air Transport
  • 3
    • 33748579291 scopus 로고    scopus 로고
    • ACARE, Advisory Council for Aeronautics Research in Europe
    • ACARE, 2000, "European Aeronautics: A vision for 2020," Advisory Council for Aeronautics Research in Europe 2000.
    • (2000) European Aeronautics: A vision for 2020
  • 9
    • 34248379765 scopus 로고    scopus 로고
    • Berrier, B. L., and Allan, A. G., 2004, Experimental and Computational Evaluation of Flush-Mounted, S-Duct Inlets, Paper No. AIAA 2004-0764.
    • Berrier, B. L., and Allan, A. G., 2004, "Experimental and Computational Evaluation of Flush-Mounted, S-Duct Inlets," Paper No. AIAA 2004-0764.
  • 14
    • 33750883696 scopus 로고    scopus 로고
    • Required Jet Area For a Silent Aircraft at Take-off
    • presented at the, Budapest University of Technology and Economics, Hungary
    • Crichton, D., Tan, D., and Hall, C. A., 2004, "Required Jet Area For a Silent Aircraft at Take-off," presented at the 8th ASC-CEAS Workshop, Budapest University of Technology and Economics, Hungary.
    • (2004) 8th ASC-CEAS Workshop
    • Crichton, D.1    Tan, D.2    Hall, C.A.3
  • 19
    • 33750857727 scopus 로고    scopus 로고
    • PANS-OPS Volume 1 Part V: Noise Abatement Procedures
    • ICAO
    • ICAO, "PANS-OPS Volume 1 Part V: Noise Abatement Procedures."
  • 22
    • 33750878568 scopus 로고
    • Acoustic and Aerodynamic Performance of a 1.83 Meter Diameter 1.25 Pressure Ratio Fan (QF-8)
    • Woodward, R. P., and Lucas, J. G., 1976, "Acoustic and Aerodynamic Performance of a 1.83 Meter Diameter 1.25 Pressure Ratio Fan (QF-8)," NASA TN D-8130 TN D-8130.
    • (1976) NASA TN , vol.D-8130 , Issue.TN
    • Woodward, R.P.1    Lucas, J.G.2
  • 23
    • 0017534279 scopus 로고
    • An Improved Correlation for the Broadband Noise of High Speed Fans
    • Ginder, R. B., and Newby, D. R., 1977, "An Improved Correlation for the Broadband Noise of High Speed Fans," J. Aircr., 14, pp. 844-849.
    • (1977) J. Aircr , vol.14 , pp. 844-849
    • Ginder, R.B.1    Newby, D.R.2
  • 26
    • 2342440179 scopus 로고
    • Interim Prediction Method for Fan and Compressor Source Noises
    • Heidmann, M. F., 1979, "Interim Prediction Method for Fan and Compressor Source Noises," NASA TM X-71763.
    • (1979) NASA TM
    • Heidmann, M.F.1
  • 29
    • 10244259214 scopus 로고    scopus 로고
    • Shockwave and Noise Abatement of Transonic Fans
    • presented at the, Vienna, Austria
    • Xu, L., 2004, "Shockwave and Noise Abatement of Transonic Fans," presented at the ASME Turbo Expo: Power for Land, Sea and Air, Vienna, Austria.
    • (2004) ASME Turbo Expo: Power for Land, Sea and Air
    • Xu, L.1
  • 30
    • 16244362004 scopus 로고    scopus 로고
    • Unsteady Aerodynamics and Aeroacoustics of a High-Bypass Ratio Fan Stage
    • Prasad, A., and Prasad, D., 2005, "Unsteady Aerodynamics and Aeroacoustics of a High-Bypass Ratio Fan Stage," ASME J. Turbomach., 127, pp. 64-75.
    • (2005) ASME J. Turbomach , vol.127 , pp. 64-75
    • Prasad, A.1    Prasad, D.2
  • 31
    • 0014808828 scopus 로고
    • Shock-Wave Radiation from a Supersonic Ducted Rotor
    • Morfey, C. L., and Fisher, M. J., 1970, "Shock-Wave Radiation from a Supersonic Ducted Rotor," Aeronaut, J., 74, pp. 579-585.
    • (1970) Aeronaut, J , vol.74 , pp. 579-585
    • Morfey, C.L.1    Fisher, M.J.2
  • 34
    • 0021411025 scopus 로고
    • Development of Controlled Diffusion Airfoils for Multistage Compressor Application
    • Hobbs, D. E., and Weingold, H. D., 1984, "Development of Controlled Diffusion Airfoils for Multistage Compressor Application," ASME J. Eng. Gas Turbines Power, 106, pp. 271-278.
    • (1984) ASME J. Eng. Gas Turbines Power , vol.106 , pp. 271-278
    • Hobbs, D.E.1    Weingold, H.D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.