Radiation and Directionality Characteristics of Advancing Side Blade-vortex Interaction (BVI) Noise

Radiation and Directionality Characteristics of Advancing Side Blade-vortex Interaction (BVI) Noise PDF Author: Fredric H. Schmitz
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Radiation and Directionality Characteristics of Advancing Side Blade-vortex Interaction (BVI) Noise

Radiation and Directionality Characteristics of Advancing Side Blade-vortex Interaction (BVI) Noise PDF Author: Fredric H. Schmitz
Publisher:
ISBN:
Category :
Languages : en
Pages :

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The Directionality of Blade-vortex Interaction Noise

The Directionality of Blade-vortex Interaction Noise PDF Author: Todd Darwin Ringler
Publisher:
ISBN:
Category :
Languages : en
Pages : 332

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Rotorcraft Blade-vortex Interaction Noise Reduction Through Attitude and Flight Parameter Variations

Rotorcraft Blade-vortex Interaction Noise Reduction Through Attitude and Flight Parameter Variations PDF Author: Juan Abelló
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Category :
Languages : en
Pages : 466

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Results of the 1986 Nasa/Faa/Dfvlr Main Rotor Test Entry in the German-Dutch Wind Tunnel (Dnw)

Results of the 1986 Nasa/Faa/Dfvlr Main Rotor Test Entry in the German-Dutch Wind Tunnel (Dnw) PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723489051
Category :
Languages : en
Pages : 24

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An acoustics test of a 40%-scale MBB BO-105 helicopter main rotor was conducted in the Deutsch-Niederlandischer Windkanal (DNW). The research, directed by NASA Langley Research Center, concentrated on the generation and radiation of broadband noise and impulsive blade-vortex interaction (BVI) noise over ranges of pertinent rotor operational envelopes. Both the broadband and BVI experimental phases are reviewed, along with highlights of major technical results. For the broadband portion, significant advancement is the demonstration of the accuracy of prediction methods being developed for broadband self noise, due to boundary layer turbulence. Another key result is the discovery of rotor blade-wake interaction (BWI) as an important contributor to mid frequency noise. Also the DNW data are used to determine for full scale helicopters the relative importance of the different discrete and broadband noise sources. For the BVI test portion, a comprehensive data base documents the BVI impulsive noise character and directionality as functions of rotor flight conditions. The directional mapping of BVI noise emitted from the advancing side as well as the retreating side of the rotor constitutes a major advancement in the understanding of this dominant discrete mechanism. Brooks, Thomas F. and Martin, Ruth M. Langley Research Center NASA-TM-100507, NAS 1.15:100507 RTOP 505-63-51-06

NASA Technical Paper

NASA Technical Paper PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 256

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Wake Geometry Effects on Rotor Blade-vortex Interaction Noise Directivity

Wake Geometry Effects on Rotor Blade-vortex Interaction Noise Directivity PDF Author: Ruth McVoy Martin
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 32

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NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 316

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Advancing-side Directivity and Retreating-side Interactions of Model Rotor Blade-vortex Interaction Noise

Advancing-side Directivity and Retreating-side Interactions of Model Rotor Blade-vortex Interaction Noise PDF Author:
Publisher:
ISBN:
Category : Acoustical engineering
Languages : en
Pages : 48

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 486

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Advancing-side Directivity and Retreating-side Interactions of Model Rotor Blade-vortex Interaction Noise

Advancing-side Directivity and Retreating-side Interactions of Model Rotor Blade-vortex Interaction Noise PDF Author: Ruth McVoy Martin
Publisher:
ISBN:
Category : Acoustical engineering
Languages : en
Pages : 48

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