1 |
Brocklehurst, A. and Pike A. C., 1994, "Reduction of BVI Noise using a Vane Tip",AHS Aeromechanics Specialists Conference Proceedings
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2 |
Murashige, A. et al., 2000, "Second ATIC Aeroacoutic Model Rotor Test at DNW",The 26th European Rotorcraft Forum Proceedings
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3 |
Leverton, J. W. and Pike, A. C., 1992, "Lynx High Perfonnance Low Noise", DGLR/ AIAA 14th Aeroocoustics Conference
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4 |
Perry F. J., Wilby P. G. and Jones A. F., 1998, "The BERP Rotor How Does It Work, and What Has It Been Doing Lately?", Vertiflite, Spring
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5 |
Beddoes, T. S. and Pike A. C., 1996, "Noise Reduction with a Twin Tip Vortex Configuration", AHS 52nd Annual Forum
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6 |
l. Gandhi, F. and Tauszig, L., 2000, "Influence of Individual Interactions on Helicopter Blade-Vortex Interaction Noise", The 26th European Rotorcraft Forum Proceedings
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7 |
Beddoes, T. S., 1985, "A Wake Model for High Resolution Airloads", Army/AHS Intemational Conference on Rotorcraft Basic Research
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8 |
Perry, F. J. et al., 1999, US Patent 5992793
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9 |
Pike, A. C., 1987, "Application of High Resolution Airload Calculations to Helicopter Noise Prediction", AHS Specialist Meeting on Aerodynamics and Aeroocoustics
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10 |
Pike, A. C., 1991, "Validation of High Frequency Airload Calculations using Full Scale Flight Test Acoustic Data", AHS/RAEs Specialist Meeting on Rotorcraft Acoustics and Rotor Fluid Dynamics
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