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Source: The Open Library
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1An analysis of shock structure and nonequilibrium laminar boundary layers induced by a normal shock wave in an ionized argon flow
By W. S. Liu
“An analysis of shock structure and nonequilibrium laminar boundary layers induced by a normal shock wave in an ionized argon flow” Metadata:
- Title: ➤ An analysis of shock structure and nonequilibrium laminar boundary layers induced by a normal shock wave in an ionized argon flow
- Author: W. S. Liu
- Publisher: ➤ Institute for Aerospace Studies
- Publish Date: 1975
- Publish Location: [Downsview, Ont.]
“An analysis of shock structure and nonequilibrium laminar boundary layers induced by a normal shock wave in an ionized argon flow” Subjects and Themes:
- Subjects: Laminar boundary layers - Argon - Nonequilibrium flow - Shock waves
Edition Identifiers:
- The Open Library ID: OL19251826M
Access and General Info:
- First Year Published: 1975
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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Source: Wikipedia
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Boundary layer
boundary layer flow: laminar and turbulent. Laminar boundary layer flow The laminar boundary is a very smooth flow, while the turbulent boundary layer contains
Boundary layer thickness
unbounded boundary layers is whether the boundary layer is being substantially influenced by more than one wall. Each of the main types has a laminar, transitional
Laminar flow
Laminar flow (/ˈlæmɪnər/) is the property of fluid particles in fluid dynamics to follow smooth paths in layers, with each layer moving smoothly past the
Boundary layer control
In engineering, boundary layer control refers to methods of controlling the behaviour of fluid flow boundary layers. It may be desirable to reduce flow
Flow separation
Boundary layers can be either laminar or turbulent. A reasonable assessment of whether the boundary layer will be laminar or turbulent can be made by calculating
Blasius boundary layer
mechanics, a Blasius boundary layer (named after Paul Richard Heinrich Blasius) describes the steady two-dimensional laminar boundary layer that forms on a
Falkner–Skan boundary layer
Falkner–Skan boundary layer (named after Victor Montague Falkner and Sylvia W. Skan) describes the steady two-dimensional laminar boundary layer that forms
Transition point
In the field of fluid dynamics the point at which the boundary layer changes from laminar to turbulent is called the transition point. Where and how this
Laminar–turbulent transition
In fluid dynamics, the process of a laminar flow becoming turbulent is known as laminar–turbulent transition. The main parameter characterizing transition
Adverse pressure gradient
characteristics. Turbulent boundary layers tend to be able to sustain an adverse pressure gradient better than an equivalent laminar boundary layer. The more efficient