Explore: Blade Slap Noise
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Reduction of Blade-Vortex Interaction (BVI) noise through X-force control
By Fredric H. Schmitz
“Reduction of Blade-Vortex Interaction (BVI) noise through X-force control” Metadata:
- Title: ➤ Reduction of Blade-Vortex Interaction (BVI) noise through X-force control
- Author: Fredric H. Schmitz
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1995
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Reduction of Blade-Vortex Interaction (BVI) noise through X-force control” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aircraft landing - Blade slap noise - Blade-vortex interaction - Flight control - Flight paths - Helicopters - Inlet flow - Longitudinal stability - Noise prediction (Aircraft) - Noise reduction
Edition Identifiers:
- The Open Library ID: OL18087419M - OL15424058M - OL17106597M - OL17117531M
- Online Computer Library Center (OCLC) ID: 35280105
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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2Helicopter blade-vortex interaction noise with comparisons to CFD calculations
By Megan S. McCluer
“Helicopter blade-vortex interaction noise with comparisons to CFD calculations” Metadata:
- Title: ➤ Helicopter blade-vortex interaction noise with comparisons to CFD calculations
- Author: Megan S. McCluer
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Helicopter blade-vortex interaction noise with comparisons to CFD calculations” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL18118604M - OL15498165M - OL17565022M - OL17125043M
- Online Computer Library Center (OCLC) ID: 39705515
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Helicopter blade-vortex interaction noise with comparisons to CFD calculations at online marketplaces:
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- Ebay: New & used books.
3Evaluation of a doubly-swept blade tip for rotorcraft noise reduction
By Brian E. Wake
“Evaluation of a doubly-swept blade tip for rotorcraft noise reduction” Metadata:
- Title: ➤ Evaluation of a doubly-swept blade tip for rotorcraft noise reduction
- Author: Brian E. Wake
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1992
- Publish Location: [Springfield, Va - Hampton, Va
“Evaluation of a doubly-swept blade tip for rotorcraft noise reduction” Subjects and Themes:
- Subjects: ➤ Rotary wings - Aeroacoustics - Blade tips - Blade slap noise - Aircraft noise - Sweep effect - Rotary wing aircraft - Blade-vortex interaction - Noise reduction - Euler equations of motion - Acoustic properties
Edition Identifiers:
- The Open Library ID: OL15413638M - OL18081154M - OL17017557M
- Online Computer Library Center (OCLC) ID: 33411839
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Evaluation of a doubly-swept blade tip for rotorcraft noise reduction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions
By William J. Devenport
“Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions” Metadata:
- Title: ➤ Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions
- Author: William J. Devenport
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - [Washington, D.C
“Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions” Subjects and Themes:
- Subjects: ➤ Blade slap noise - Blade-vortex interaction - Helicopters - Noise prediction - Rotary wings - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15413882M - OL17633128M - OL17791704M
- Online Computer Library Center (OCLC) ID: 33450830 - 32031695
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
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5The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction
By William J. Devenport
“The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction” Metadata:
- Title: ➤ The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction
- Author: William J. Devenport
- Language: English
- Publisher: ➤ Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC - Blacksburg, VA
“The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction” Subjects and Themes:
- Subjects: ➤ Helicopters - Rotary wings - Aeroacoustics - Blade tips - Blade slap noise - Statistical distributions - Noise prediction - Blade-vortex interaction - Aerodynamic noise - Turbulent wakes - Interactional aerodynamics - Incompressible flow
Edition Identifiers:
- The Open Library ID: OL15479176M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6UHB engine fan broadband noise reduction study
By Philip R. Gliebe
“UHB engine fan broadband noise reduction study” Metadata:
- Title: ➤ UHB engine fan broadband noise reduction study
- Author: Philip R. Gliebe
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“UHB engine fan broadband noise reduction study” Subjects and Themes:
- Subjects: ➤ Fan blades - Noise reduction - Blade slap noise - Engine tests - Broadband - Flight simulators - Turbine wheels - Turbofan engines - Noise generators - Engine noise
Edition Identifiers:
- The Open Library ID: OL15414971M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find UHB engine fan broadband noise reduction study at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.