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Air Travel - Greener by design: The Technology Challenge
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2
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Department for Transport, UK Government
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3
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33748579291
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5
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0003567466
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9
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11
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NASA CR-2003-212309
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Daggett, D. L., Brown, S. T., and Kawai, R. T., 2003, "Ultra-Efficient Engine Diameter Study," NASA CR-2003-212309.
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Ultra-Efficient Engine Diameter Study
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Daggett, D.L.1
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13
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34248395661
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NASA TM-2003-212322
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Dittmar, J. H., Tweedt, D., Jeracki, R., Envia, E., Bartos, K., and Slater, J., 2003, "A Fan Design That Meets the NASA Aeronautics Noise Goals," NASA TM-2003-212322.
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14
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33750883696
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Required Jet Area For a Silent Aircraft at Take-off
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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.
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8th ASC-CEAS Workshop
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PANS-OPS Volume 1 Part V: Noise Abatement Procedures
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ICAO
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ICAO, "PANS-OPS Volume 1 Part V: Noise Abatement Procedures."
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22
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33750878568
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Acoustic and Aerodynamic Performance of a 1.83 Meter Diameter 1.25 Pressure Ratio Fan (QF-8)
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Woodward, R.P.1
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0017534279
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An Improved Correlation for the Broadband Noise of High Speed Fans
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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.
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ASME Paper No. GT2005-68573
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Hughes, C. E., Woodward, R. P., Podboy, G. G., and Jeracki, R. J., 2005, "The Effect of Bypass Nozzle Exit Area on Fan Aerodynamic Performance and Noise in a Model Turbofan Simulator," ASME Paper No. GT2005-68573.
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The Effect of Bypass Nozzle Exit Area on Fan Aerodynamic Performance and Noise in a Model Turbofan Simulator
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Hughes, C.E.1
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25
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84896690836
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Woodward, R. P., Hughes, C. E., Jeracki, R., and Miller, C. J., 2002, "Fan Noise Source Diagnostic Test - Far Field Acoustic Results," presented at the 8th AIAA/CEAS Aeroacoustics Conference & Exhibit, Breckenridge, CO.
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8th AIAA/CEAS Aeroacoustics Conference & Exhibit
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Woodward, R.P.1
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26
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2342440179
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Interim Prediction Method for Fan and Compressor Source Noises
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28
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34248376162
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Inch Low Noise Research Fan Rig Preliminary Design of ADP-Type Fan, NASA CR-2004-212718
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Topol, D. A., Ingram, C. L., Larkin, M. J., Roche, C. H., and Thulin, R. D., 2004, "Advanced Subsonic Technology (AST) 22-Inch Low Noise Research Fan Rig Preliminary Design of ADP-Type Fan 3," NASA CR-2004-212718.
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Shockwave and Noise Abatement of Transonic Fans
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Xu, L., 2004, "Shockwave and Noise Abatement of Transonic Fans," presented at the ASME Turbo Expo: Power for Land, Sea and Air, Vienna, Austria.
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ASME Turbo Expo: Power for Land, Sea and Air
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Xu, L.1
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30
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16244362004
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Unsteady Aerodynamics and Aeroacoustics of a High-Bypass Ratio Fan Stage
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31
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Development of Controlled Diffusion Airfoils for Multistage Compressor Application
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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.
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Hobbs, D.E.1
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