Explore: Supersonic Boundary Layers
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Source: The Open Library
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1Supersonic laminar flow control research
By Ching F. Lo
“Supersonic laminar flow control research” Metadata:
- Title: ➤ Supersonic laminar flow control research
- Author: Ching F. Lo
- Language: English
- Publisher: ➤ Ames Research Center - National Aeronautics and Space Administration - University of Tennessee, Space Institute - National Technical Information Service, distributor
- Publish Date: 1995 - 1996
- Publish Location: ➤ Tullahoma, TN - [Springfield, Va - Moffett Field, CA - [Washington, DC - Springfield, Va
“Supersonic laminar flow control research” Subjects and Themes:
- Subjects: ➤ Boundary layer stability - Supersonic boundary layers - Boundary layer control - Supersonic flow - Laminar flow - Active control - Computational fluid dynamics - Control systems design - Boundary layer flow - Laminar boundary layer - Boundary layer transition - Wind tunnel nozzles - Stability - Temperature distribution - Wind tunnel tests - Laminar boundary - Wall temperature - Supersonic wind tunnels - Prediction analysis techniques - Nozzle design
Edition Identifiers:
- The Open Library ID: OL15543412M - OL15424662M - OL15506457M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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2High-order polynomial expansions (HOPE) for flux-vector splitting
By M. S. Liou
“High-order polynomial expansions (HOPE) for flux-vector splitting” Metadata:
- Title: ➤ High-order polynomial expansions (HOPE) for flux-vector splitting
- Author: M. S. Liou
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1991
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“High-order polynomial expansions (HOPE) for flux-vector splitting” Subjects and Themes:
- Subjects: ➤ Viscous flow - Hypersonic flow - Polynomials - Navier-Stokes equation - Supersonic boundary layers - Conical flow - Flux vector splitting - Shock waves
Edition Identifiers:
- The Open Library ID: OL17114482M - OL15407296M - OL18078165M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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3Embedded function methods for compressible high speed turbulent flow
By J. D. A. Walker
“Embedded function methods for compressible high speed turbulent flow” Metadata:
- Title: ➤ Embedded function methods for compressible high speed turbulent flow
- Author: J. D. A. Walker
- Language: English
- Publisher: NASA Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va
“Embedded function methods for compressible high speed turbulent flow” Subjects and Themes:
- Subjects: ➤ Compressible flow - Computational fluid dynamics - Supersonic boundary layers - Supersonic flow - Turbulent boundary layer - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL17790660M - OL15408583M
- Online Computer Library Center (OCLC) ID: 32668807
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Non-linear evolution of a second mode wave in supersonic boundary layers
By Gordon Erlebacher
“Non-linear evolution of a second mode wave in supersonic boundary layers” Metadata:
- Title: ➤ Non-linear evolution of a second mode wave in supersonic boundary layers
- Author: Gordon Erlebacher
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1989
- Publish Location: [Springfield, Va - Hampton, VA
“Non-linear evolution of a second mode wave in supersonic boundary layers” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary value problems - Computerized simulation - Supersonic boundary layers - Channel flow - Flow stability - Wall flow - Boundary layer transition - Wave generation - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15407774M - OL18078350M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Laser Doppler vellcimeter measurements of boundary layer velocity and turbulent intensities in MACH 2.5 flow
By Jesse Sewell
“Laser Doppler vellcimeter measurements of boundary layer velocity and turbulent intensities in MACH 2.5 flow” Metadata:
- Title: ➤ Laser Doppler vellcimeter measurements of boundary layer velocity and turbulent intensities in MACH 2.5 flow
- Author: Jesse Sewell
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - University of Central Florida, Dept. of Mechanical and Aerospace Engineering
- Publish Date: 1994
- Publish Location: ➤ Orlando, Fla - Springfield, Va - [Washington, DC
“Laser Doppler vellcimeter measurements of boundary layer velocity and turbulent intensities in MACH 2.5 flow” Subjects and Themes:
- Subjects: Flow velocity - Laser Doppler velocimeters - Particle image velocimetry - Supersonic boundary layers - Turbulent boundary layer
Edition Identifiers:
- The Open Library ID: OL15403980M - OL17790277M
- Online Computer Library Center (OCLC) ID: 32259311
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6On the coupling between a supersonic boundary layer and a flexible surface
By Abdelkader Frendi
“On the coupling between a supersonic boundary layer and a flexible surface” Metadata:
- Title: ➤ On the coupling between a supersonic boundary layer and a flexible surface
- Author: Abdelkader Frendi
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1992 - 1996
- Publish Location: Hampton, Va - [Springfield, Va
“On the coupling between a supersonic boundary layer and a flexible surface” Subjects and Themes:
- Subjects: ➤ Equilibrium of flexible surfaces - Turbulent boundary layer - Aircraft structures - Flexible bodies - Mathematical models - Computer programs - Supersonic boundary layers - Boundary layer - Mach number - Absorbers (Materials)
Edition Identifiers:
- The Open Library ID: OL14686485M - OL15487233M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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7The development of a mass flow probe
By E. R. Wolff
“The development of a mass flow probe” Metadata:
- Title: ➤ The development of a mass flow probe
- Author: E. R. Wolff
- Number of Pages: Median: 18
- Publisher: ➤ Dept. of Aeronautical Engineering and Aerophysics - Institute of Aerophysics
- Publish Date: 1957
- Publish Location: [Downsview, Ont.]
“The development of a mass flow probe” Subjects and Themes:
- Subjects: Mass flow - Probes - Supersonic boundary layers
Edition Identifiers:
- The Open Library ID: OL19003977M - OL20983007M
Access and General Info:
- First Year Published: 1957
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point
By V. I. Lysenko
“Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point” Metadata:
- Title: ➤ Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point
- Author: V. I. Lysenko
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point” Subjects and Themes:
- Subjects: Boundary layer stability - Laminar boundary layer - Turbulent boundary layer - Transition flow - Supersonic boundary layers
Edition Identifiers:
- The Open Library ID: OL17116065M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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9A near-wall two-equation model for compressible turbulent flows
By H. S. Zhang
“A near-wall two-equation model for compressible turbulent flows” Metadata:
- Title: ➤ A near-wall two-equation model for compressible turbulent flows
- Author: H. S. Zhang
- Number of Pages: Median: 35
- Publisher: ➤ Institute for Computer Applications in Science and Engineering
- Publish Date: 1991
- Publish Location: Hampton, Va
“A near-wall two-equation model for compressible turbulent flows” Subjects and Themes:
- Subjects: Supersonic boundary layers - Turbulence models - Compressible flow
Edition Identifiers:
- The Open Library ID: OL21378439M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10On the modulational instability of large amplitude waves in supersonic boundary layers
By Philip Hall
“On the modulational instability of large amplitude waves in supersonic boundary layers” Metadata:
- Title: ➤ On the modulational instability of large amplitude waves in supersonic boundary layers
- Author: Philip Hall
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, VA - [Springfield, Va
“On the modulational instability of large amplitude waves in supersonic boundary layers” Subjects and Themes:
- Subjects: Boundary layer stability - Compressible boundary layer - Mach number - Supersonic boundary layers - Tollmien-Schlichting waves
Edition Identifiers:
- The Open Library ID: OL15413656M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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11Non-linear evolution of a second mode wave in supersonic boundary layers
By Gordon Erlebacher
“Non-linear evolution of a second mode wave in supersonic boundary layers” Metadata:
- Title: ➤ Non-linear evolution of a second mode wave in supersonic boundary layers
- Author: Gordon Erlebacher
- Number of Pages: Median: 37
- Publisher: ICASE
- Publish Date: 1989
- Publish Location: Hampton, Va
“Non-linear evolution of a second mode wave in supersonic boundary layers” Subjects and Themes:
- Subjects: Stability - Supersonic boundary layers - Transition - Compressible boundary layers
Edition Identifiers:
- The Open Library ID: OL18931487M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer
By Abdelkader Frendi
“Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer” Metadata:
- Title: ➤ Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer
- Author: Abdelkader Frendi
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: Hampton, Va - [Springfield, Va
“Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer” Subjects and Themes:
- Subjects: Pressure gradients - Supersonic boundary layers - Turbulent boundary layer - High frequencies - Boundary layer thickness
Edition Identifiers:
- The Open Library ID: OL15505121M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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13Numerical simulation of supersonic flow using a new analytical bleed boundary condition
By G. J. Harloff
“Numerical simulation of supersonic flow using a new analytical bleed boundary condition” Metadata:
- Title: ➤ Numerical simulation of supersonic flow using a new analytical bleed boundary condition
- Author: G. J. Harloff
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Numerical simulation of supersonic flow using a new analytical bleed boundary condition” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Supersonic boundary layers - Supersonic flow - Flow distribution - Oblique shock waves - Boundary layer control - Supersonic inlets - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15381444M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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