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Flight dynamics-Concepts, quantities and symbols-Part 1: Aircraft motion relative to the air
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International Organization for Standardization
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2
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Flight dynamics-Concepts, quantities and symbols-Part 2: Motions of the aircraft and the atmosphere relative to the Earth
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Berlin, Germany , October
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4
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Validation of ONERA Aeroacoustic Prediction Methods for Blade-Vortex Interaction using Hart Tests Results
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Fort Worth, Texas, USA , May
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"Prediction and Measurement of Blade-Vortex Interaction"
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Effect of Wake Structure on Blade-Vortex Interaction Phenomena: Acoustic Prediction and Validation
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"The HART-II Test: Rotor Wakes and Aeroacoustics with Higher-Harmonic Pitch Control (HHC) Inputs-The Joint German/French/Dutch/US Project"
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Montreal, Canada , June
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Yu, Y. H.; Tung, C.; van der Wall, B.; Pausder, H.- J.; Burley, C. L.; Brooks, T. F.; Beaumier, P.; Delrieux, Y.; Mercker, E. and Pengel, K., "The HART-II Test: Rotor Wakes and Aeroacoustics with Higher-Harmonic Pitch Control (HHC) Inputs-The Joint German/French/Dutch/US Project", American Helicopter Society 58th Annual Forum, Montreal, Canada , June 2002.
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BVI Noise Prediction using a Comprehensive Rotorcraft Analysis
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Washington D.C., USA, May
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Noise Prediction For Maneuvering Rotorcraft
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A New Aerodynamic & Acoustic Computation Chain for BVI Noise Prediction in Unsteady Flight Conditions
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Baltimore, MD, USA , June
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Perez, G.1
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Acoustic Directivity of Maneuvering Helicopters Using Wave Tracing Concepts
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Operational Tests of Noise Abatement Approaches for Rotorcraft Using Differential GPS for Guidance
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The Development and Flight Test Demonstration of Noise Abatement Approach Procedures for the Sikorsky S-76
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Jacobs, E. W.; Prillwitz, R. D.; Chen, R. T. N. and Hindson, W. S., "The Development and Flight Test Demonstration of Noise Abatement Approach Procedures for the Sikorsky S-76", American Helicopter Society Technical Specialists Meeting For Rotorcraft Acoustics and Aerodynamics, October 1997.
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Acoustic Flight Testing of a Boeing MD Explorer and a Sikorsky S-76B using a Large Area Microphone Array
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Development and Demonstration of Noise Abatement Approach Flight Operations for a Light Twin-engine Helicopter-MD Explorer
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October
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A New Technique for Estimating Ground Footprint Acoustics for Rotorcraft using measured Sound Fields
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Environmental Noise Modelling for UK Military Helicopter Training Operations
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Phoenix, Arizona, USA , May
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33745530621
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Towards Noise Abatement Flight Procedure Design: DLR Rotorcraft Noise Ground Footprint Model and its Validation
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France , September
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85029787043
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Helicopter Rotor Blade Aeroacoustics: A Comparison of Model- Scale Wind Tunnel and Full-Scale Flight Test Results
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The "RONAP" Aeroacoustic Flight Tests with a Highly Instrumented BO 105 Helicopter
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Spiegel, P.; Buchholz, H. and Splettstoesser, W., "The "RONAP" Aeroacoustic Flight Tests with a Highly Instrumented BO 105 Helicopter", American Helicopter Society 59th Annual Forum, Phoenix, Arizona , May 2003.
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33644667980
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FHS, the New Research Helicopter: Ready for Service
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Kaletka, J.; Kurscheid, H. and Butter, U., "FHS, the New Research Helicopter: Ready for Service", 29th European Rotorcraft Forum, Friedrichshafen, Germany , September 2003.
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Pilot assistant-the next generation helicopter cockpit
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BVI Noise Prediction Starting from Blade Pressures Measured at Few Points"
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Full Scale Rotor Aeroacoustic Predicition and the Link to Model Scale Rotor Data
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Eichung einer Siebenloch-Sonde zur Messung der Strömungsgeschwindigkeit nach Größe und Richtung
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Key Results from a Higher Harmonic Control Aeroacoustic Rotor Test (HART)
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HART II Blade Motion Measured by Stereo Pattern Recognition (SPR)
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Phoenix, AZ, USA , May
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Schneider, O. and van der Wall, B., "HART II Blade Motion Measured by Stereo Pattern Recognition (SPR)", American Helicopter Society 59th Annual Forum, Phoenix, AZ, USA , May 2003.
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HOST: A General Helicopter Simulation Tool for Germany and France
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Virginia Beach, Virginia, USA , May
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