Explore: *flow Separation
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Fully nonlinear Gortler vortices in constricted channel flows and their effect on the onset of separation
By James P. Denier
“Fully nonlinear Gortler vortices in constricted channel flows and their effect on the onset of separation” Metadata:
- Title: ➤ Fully nonlinear Gortler vortices in constricted channel flows and their effect on the onset of separation
- Author: James P. Denier
- Number of Pages: Median: 31
- Publisher: ➤ Institute for Computer Applications in Science and Engineering
- Publish Date: 1992
- Publish Location: Hampton, Va
“Fully nonlinear Gortler vortices in constricted channel flows and their effect on the onset of separation” Subjects and Themes:
- Subjects: Flow separation - Gortler vortices
Edition Identifiers:
- The Open Library ID: OL19245938M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Experimental and computational analysis of separation bubble behavior for compressible, steady and oscillatory flows over a NACA 0012 airfoil at M=0.3 and a reynolds number of 540,000
By Robert D. Van Dyken

“Experimental and computational analysis of separation bubble behavior for compressible, steady and oscillatory flows over a NACA 0012 airfoil at M=0.3 and a reynolds number of 540,000” Metadata:
- Title: ➤ Experimental and computational analysis of separation bubble behavior for compressible, steady and oscillatory flows over a NACA 0012 airfoil at M=0.3 and a reynolds number of 540,000
- Author: Robert D. Van Dyken
- Language: English
- Number of Pages: Median: 180
- Publisher: Naval Postgraduate School
- Publish Date: 1997
- Publish Location: Monterey, California
“Experimental and computational analysis of separation bubble behavior for compressible, steady and oscillatory flows over a NACA 0012 airfoil at M=0.3 and a reynolds number of 540,000” Subjects and Themes:
- Subjects: VORTEX SHEDDING - STALLING - FLOW SEPARATION - BUBBLES
Edition Identifiers:
- The Open Library ID: OL25311390M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: Yes
- Is The Book Public: Yes
- Access Status: Public
Online Access
Online Borrowing:
- Borrowing from Open Library: Borrowing link
- Borrowing from Archive.org: Borrowing link
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Find Experimental and computational analysis of separation bubble behavior for compressible, steady and oscillatory flows over a NACA 0012 airfoil at M=0.3 and a reynolds number of 540,000 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Flow separation
In fluid dynamics, flow separation or boundary layer separation is the detachment of a boundary layer from a surface into a wake. A boundary layer exists
Axial compressor
engine power. Positive stalling Flow separation occur on the suction side of the blade. Negative stalling Flow separation occur on the pressure side of
Drag coefficient
from the surface of the object. At very low Reynolds numbers, without flow separation, the drag force F d {\displaystyle F_{\mathrm {d} }} is proportional
Stall (fluid dynamics)
at which the maximum lift coefficient occurs. Stalling is caused by flow separation which, in turn, is caused by the air flowing against a rising pressure
Wake (physics)
recirculating flow immediately behind a moving or stationary blunt body, caused by viscosity, which may be accompanied by flow separation and turbulence
Adverse pressure gradient
even become reversed causing a flow separation. This has very significant consequences in aerodynamics since flow separation significantly modifies the pressure
Flow Separation
Flow Separation is a red and white, marbled repainting of the John J. Harvey fireboat by artist Tauba Auerbach. The project was a collaboration with the
D'Alembert's paradox
streamlined objects, and for bluff bodies the additional result is flow separation and a low-pressure wake behind the object, leading to form drag. The
Unidirectional data flow
unidirectional data flow. Separation of state changes from presentation has many benefits and was popularized with Redux for unidirectional data flow combined with
Delta wing
sufficiently high angle the wing exhibits flow separation, together with an associated high drag. Ordinarily, this flow separation leads to a loss of lift known as