Author: Fredric H. Schmitz
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Radiation and Directionality Characteristics of Advancing Side Blade-vortex Interaction (BVI) Noise
Author: Fredric H. Schmitz
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
The Directionality of Blade-vortex Interaction Noise
Author: Todd Darwin Ringler
Publisher:
ISBN:
Category :
Languages : en
Pages : 332
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 332
Book Description
Rotorcraft Blade-vortex Interaction Noise Reduction Through Attitude and Flight Parameter Variations
Author: Juan Abelló
Publisher:
ISBN:
Category :
Languages : en
Pages : 466
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 466
Book Description
Results of the 1986 Nasa/Faa/Dfvlr Main Rotor Test Entry in the German-Dutch Wind Tunnel (Dnw)
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723489051
Category :
Languages : en
Pages : 24
Book Description
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
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723489051
Category :
Languages : en
Pages : 24
Book Description
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
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 256
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 256
Book Description
Wake Geometry Effects on Rotor Blade-vortex Interaction Noise Directivity
Author: Ruth McVoy Martin
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 32
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 316
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 316
Book Description
Advancing-side Directivity and Retreating-side Interactions of Model Rotor Blade-vortex Interaction Noise
Author:
Publisher:
ISBN:
Category : Acoustical engineering
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Acoustical engineering
Languages : en
Pages : 48
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 486
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 486
Book Description
Advancing-side Directivity and Retreating-side Interactions of Model Rotor Blade-vortex Interaction Noise
Author: Ruth McVoy Martin
Publisher:
ISBN:
Category : Acoustical engineering
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Acoustical engineering
Languages : en
Pages : 48
Book Description