Explore: Blade Slap Noise
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AI-Generated Overview About “blade-slap-noise”:
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
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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:
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- 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
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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.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
3 (American band)
on Planet Noise Records, a small indie label, and thenceforth managed themselves independently, until their 2005 signing with Metal Blade, on whose label
Clapper (musical instrument)
handles and hits the two pieces of wood together, creating a loud whip noise. The other type also has two planks of wood, one longer than the other,
Scott Burns (music producer)
Eulogy for a Dying Fetus in the Metal Archives Arise in the Metal Archives Slap Of Reality – Fletch in Discogs The Ten Commandments in the Metal Archives
Sharpie (boat)
2 inches deep, which were then rounded into a shallow arc. The noise is the same as chine slap familiar to owners of deep-V powerboats at anchor. Other designers
Diamond grinding of pavement
improvement in skid resistance, noise reduction and safety. The industry can be traced back to an event where a single diamond blade mounted on a concrete saw
Strike (attack)
the bicep of the right arm, as you add more power and speed you end up slapping your bicep on the way by. A strike using the part of the hand opposite
Cavitation
concrete propeller example: The pressure on the suction side of the propeller blades can be very low and when the pressure falls to that of the vapour pressure
Revenge (2017 film)
When Jen threatens to reveal their relationship to Richard's wife, Richard slaps her, and she runs off into the desert, pursued by the three men. Richard
Alton Towers
Bambrough, Billy (27 September 2016). "Alton Towers owner Merlin just got slapped with a £5m fine". Retrieved 28 October 2024. "Alton Towers owner and multi-millionaire
AKM
last few millimeters of forward movement. The device also reduces "trigger slap" or "trigger bounce" and the weapon's rate of fire, which also reduces the