Explore: Boundary Layer Separation
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Source: The Open Library
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1Numerical solutions of the complete Navier-Stokes equations
By H. A. Hassan
“Numerical solutions of the complete Navier-Stokes equations” Metadata:
- Title: ➤ Numerical solutions of the complete Navier-Stokes equations
- Author: H. A. Hassan
- Language: English
- Publisher: ➤ Dept. of Mechanical and Aerospace Engineering, North Carolina State University - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1989 - 1994 - 1995 - 1996
- Publish Location: ➤ [Washington, DC - [Washington, D.C - Raleigh, N.C - Springfield, Va
“Numerical solutions of the complete Navier-Stokes equations” Subjects and Themes:
- Subjects: ➤ Navier-Stokes equation - Turbulent flow - Turbulence models - Eddy viscosity - Flow velocity - Supersonic combustion - Mixing layers (Fluids) - Jet flow - Navier-Stokes equations - Compressible flow - Compressibility - Numerical solutions - Turbulent mixing - Computational fluid dynamics - Numerical analysis - Vorticity - Boundary layer separation - Vortices - Pressure gradients - Three dimensional flow - Aerodynamic characteristics - Airfoils
Edition Identifiers:
- The Open Library ID: OL15419184M - OL15452379M - OL16135487M - OL14706079M
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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2Control of low-speed turbulent separated flow over a backward-facing ramp
By John C. Lin
“Control of low-speed turbulent separated flow over a backward-facing ramp” Metadata:
- Title: ➤ Control of low-speed turbulent separated flow over a backward-facing ramp
- Author: John C. Lin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Control of low-speed turbulent separated flow over a backward-facing ramp” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Separated flow - Boundary layer separation - Vortices - Flow characteristics - Vortex generators - Horseshoe vortices - Vortex shedding - Low speed - Angle of attack - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL18075631M - OL15402173M - OL17000678M - OL17113743M
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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3Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations
By David A. Boger
“Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations” Metadata:
- Title: ➤ Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations
- Author: David A. Boger
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations” Subjects and Themes:
- Subjects: ➤ Viscous flow - Turbulent flow - Boundary layer separation - Low Reynolds number - Vortex generators - Predictions - Navier-Stokes equation - Engine inlets - Aircraft engines - K-epsilon turbulence model
Edition Identifiers:
- The Open Library ID: OL17122720M - OL18116007M - OL15491180M - OL17540932M
- Online Computer Library Center (OCLC) ID: 38840668
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Vortex flow aerodynamics
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Vortex flow aerodynamics” Metadata:
- Title: Vortex flow aerodynamics
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 534
- Publisher: AGARD
- Publish Date: 1991
- Publish Location: ➤ Neuilly-sur-Seine - Neuilly sur Seine, France
“Vortex flow aerodynamics” Subjects and Themes:
- Subjects: Boundary layer separation - Fighter aircraft - Vortex generators - Vortices
Edition Identifiers:
- The Open Library ID: OL20116993M - OL21500079M
- All ISBNs: 9283506235 - 9789283506232
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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5Control of unsteady separated flow associated with the dynamic stall of airfoils
By Michael C. Wilder
“Control of unsteady separated flow associated with the dynamic stall of airfoils” Metadata:
- Title: ➤ Control of unsteady separated flow associated with the dynamic stall of airfoils
- Author: Michael C. Wilder
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - MCAT Institute
- Publish Date: 1992 - 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - Springfield, Va.? - San Jose, CA
“Control of unsteady separated flow associated with the dynamic stall of airfoils” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Wind tunnel tests - Leading edges - Aerodynamic stalling - Boundary layer control - Unsteady flow (Aerodynamics) - Separated flow - Boundary layer separation - Reynolds number - Supercritical airfoils - Airfoil oscillations - Airfoil profiles - Airfoils - Mach number - Active control
Edition Identifiers:
- The Open Library ID: OL15365679M - OL15408283M - OL15415078M
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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6Computation of Navier-Stokes equations for three-dimensional flow separation
By Ching-Mao Hung
“Computation of Navier-Stokes equations for three-dimensional flow separation” Metadata:
- Title: ➤ Computation of Navier-Stokes equations for three-dimensional flow separation
- Author: Ching-Mao Hung
- Language: English
- Number of Pages: Median: 19
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1989
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Computation of Navier-Stokes equations for three-dimensional flow separation” Subjects and Themes:
- Subjects: ➤ Fluid dynamics - Mathematical models - Computational fluid dynamics - Flat plates - Boundary layer separation - Supersonic flow - Flow distribution
Edition Identifiers:
- The Open Library ID: OL18263481M - OL17630346M - OL16138491M
- Online Computer Library Center (OCLC) ID: 25291040
Author's Alternative Names:
"Ching-mao Hung"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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7Unsteady three-dimensional marginal separation, including breakdown
By Peter W. Duck
“Unsteady three-dimensional marginal separation, including breakdown” Metadata:
- Title: ➤ Unsteady three-dimensional marginal separation, including breakdown
- Author: Peter W. Duck
- Language: English
- Number of Pages: Median: 29
- Publisher: ➤ Institute for Computational Mechanics in Propulsion, NASA Lewis Research Center, Case Western Reserve University - NASA - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Cleveland, Ohio] - [Washington, D.C.] - [Springfield, Va
“Unsteady three-dimensional marginal separation, including breakdown” Subjects and Themes:
- Subjects: ➤ Mathematical models - Boundary layer - Three dimensional models - Separated flow - Boundary layer separation - Steady flow - Spectral methods
Edition Identifiers:
- The Open Library ID: OL17630434M - OL18257090M - OL16135158M
- Online Computer Library Center (OCLC) ID: 25073385
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
By David S. Dolling
“Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction” Metadata:
- Title: ➤ Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
- Author: David S. Dolling
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Austin, Tex - [Washington, DC
“Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Unsteady flow - Boundary layer separation - Aerodynamic loads - Corner flow - Vortex generators - Hypersonic boundary layer - Boundary layer control - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL18088579M - OL17803977M - OL15425915M
- Online Computer Library Center (OCLC) ID: 35454133
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Enhanced design of turbo-jet LPT by separation control using phased plasma actuators
By Thomas C. Corke
“Enhanced design of turbo-jet LPT by separation control using phased plasma actuators” Metadata:
- Title: ➤ Enhanced design of turbo-jet LPT by separation control using phased plasma actuators
- Author: Thomas C. Corke
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - Available from NASA Center for Aerospace Administration - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2003
- Publish Location: ➤ Springfield, VA - Hanover, MD - [Cleveland, Ohio]
“Enhanced design of turbo-jet LPT by separation control using phased plasma actuators” Subjects and Themes:
- Subjects: ➤ Actuators - Boundary layer separation - Computational fluid dynamics - Flow distribution - Pressure distribution - Reattached flow - Separated flow - Turbine blades
Edition Identifiers:
- The Open Library ID: OL17633155M - OL18205099M - OL16094177M
- Online Computer Library Center (OCLC) ID: 56823171
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10The three dimensional flow field at the exit of an axial-flow turbine rotor
By B. Lakshminarayana
“The three dimensional flow field at the exit of an axial-flow turbine rotor” Metadata:
- Title: ➤ The three dimensional flow field at the exit of an axial-flow turbine rotor
- Author: B. Lakshminarayana
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“The three dimensional flow field at the exit of an axial-flow turbine rotor” Subjects and Themes:
- Subjects: ➤ Viscous flow - Fluid dynamics - Boundary layer separation - Blade tips - Three dimensional flow - Spatial resolution - Axial flow turbines - Vorticity - Wakes
Edition Identifiers:
- The Open Library ID: OL15544533M - OL17597293M
- Online Computer Library Center (OCLC) ID: 41899970
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Computation of three-dimensional boundary layers including separation
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Computation of three-dimensional boundary layers including separation” Metadata:
- Title: ➤ Computation of three-dimensional boundary layers including separation
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Publisher: Sine nomine - AGARD
- Publish Date: 1987
- Publish Location: ➤ S.l - Neuilly sur Seine, France
“Computation of three-dimensional boundary layers including separation” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Boundary layer flow - Boundary layer separation - Boundary layer transition - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL21697122M - OL18999282M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Special course on three-dimensional supersonic/hypersonic flows including separation
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Special course on three-dimensional supersonic/hypersonic flows including separation” Metadata:
- Title: ➤ Special course on three-dimensional supersonic/hypersonic flows including separation
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 394
- Publisher: AGARD
- Publish Date: 1990
- Publish Location: ➤ Neuilly-sur-Seine - Neuilly sur Seine, France
“Special course on three-dimensional supersonic/hypersonic flows including separation” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL20124782M - OL21039442M
- All ISBNs: 9789283505372 - 9283505379
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Calculation of 3D separated turbulent flows in boundary layer limit
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Calculation of 3D separated turbulent flows in boundary layer limit” Metadata:
- Title: ➤ Calculation of 3D separated turbulent flows in boundary layer limit
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 143
- Publisher: AGARD
- Publish Date: 1990
- Publish Location: ➤ Neuilly-sur-Seine - Neuilly sur Seine, France
“Calculation of 3D separated turbulent flows in boundary layer limit” Subjects and Themes:
- Subjects: Boundary layer separation - Three dimensional flow - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL21333476M - OL20124804M
- All ISBNs: 9789283505600 - 9283505603
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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14Control of flow separation and mixing by aerodynamic excitation
By Edward J. Rice
“Control of flow separation and mixing by aerodynamic excitation” Metadata:
- Title: ➤ Control of flow separation and mixing by aerodynamic excitation
- Author: Edward J. Rice
- Language: English
- Number of Pages: Median: 11
- Publisher: ➤ NASA - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Control of flow separation and mixing by aerodynamic excitation” Subjects and Themes:
- Subjects: ➤ Shear flow - Inlet flow - Shear layers - Separated flow - Boundary layer separation - Coanda effect - Engine inlets - Aircraft engines - Airfoils - Mixing - Turbulence effects - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL16135113M - OL17634399M
- Online Computer Library Center (OCLC) ID: 24985892
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15Low speed analysis of mission adaptive flaps on a high speed civil transport configuration
By Victor R. Lessard
“Low speed analysis of mission adaptive flaps on a high speed civil transport configuration” Metadata:
- Title: ➤ Low speed analysis of mission adaptive flaps on a high speed civil transport configuration
- Author: Victor R. Lessard
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“Low speed analysis of mission adaptive flaps on a high speed civil transport configuration” Subjects and Themes:
- Subjects: ➤ Baldwin-Lomax turbulence model - Boundary layer separation - Flapping - Leading edge flaps - Low speed - Mathematical models - Pitching moments - Thin films - Turbulence models
Edition Identifiers:
- The Open Library ID: OL15567867M - OL17595195M
- Online Computer Library Center (OCLC) ID: 44114595
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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163D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By M. Mizukami
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Author: M. Mizukami
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Supersonic diffusers - Computational grids - Boundary layer separation - Turbulence models - Three dimensional flow - Flow distribution - Engine inlets - Internal flow - Leading edges - Shock wave interaction - Navier-Stokes equation - Shock waves
Edition Identifiers:
- The Open Library ID: OL17117540M - OL17106503M
- Online Computer Library Center (OCLC) ID: 35282961
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
By Dale Ashby
“Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil” Metadata:
- Title: ➤ Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
- Author: Dale Ashby
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Joint Institute for Aeronautics and Acoustics, Stanford University - National Technical Information Service, distributor - Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1996
- Publish Location: ➤ [Stanford, Calif.] - [Washington, DC - Springfield, Va
“Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Airfoils - Boundary layer separation - Flaps (Control surfaces) - Incompressible flow - Lift augmentation - Potential flow - Pressure distribution - Separated flow - Tabs (Control surfaces)
Edition Identifiers:
- The Open Library ID: OL15505042M - OL17838000M
- Online Computer Library Center (OCLC) ID: 40101894
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Experimental study of boundary layer behavior in a simulated low pressure turbine
By Rickey J. Shyne
“Experimental study of boundary layer behavior in a simulated low pressure turbine” Metadata:
- Title: ➤ Experimental study of boundary layer behavior in a simulated low pressure turbine
- Author: Rickey J. Shyne
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Experimental study of boundary layer behavior in a simulated low pressure turbine” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Turbulent boundary layer - Fluid dynamics - Boundary layer separation - Wind tunnel tests - Turbines - Low pressure - Flow visualization - Boundary layer transition - Flow measurement
Edition Identifiers:
- The Open Library ID: OL17839326M - OL15546581M
- Online Computer Library Center (OCLC) ID: 41553970
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Stability of separating subsonic boundary layers
By Jamal A. Masad
“Stability of separating subsonic boundary layers” Metadata:
- Title: ➤ Stability of separating subsonic boundary layers
- Author: Jamal A. Masad
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va - Springfield, VA
“Stability of separating subsonic boundary layers” Subjects and Themes:
- Subjects: Surface roughness - Boundary layer flow - Boundary layer separation - Laminar flow - Flow stability
Edition Identifiers:
- The Open Library ID: OL17790640M - OL15409742M
- Online Computer Library Center (OCLC) ID: 32801791
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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203D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By Masashi Mizukami
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Author: Masashi Mizukami
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Supersonic diffusers - Computational grids - Boundary layer separation - Turbulence models - Three dimensional flow - Flow distribution - Engine inlets - Internal flow - Leading edges - Shock wave interaction - Navier-Stokes equation - Shock waves
Edition Identifiers:
- The Open Library ID: OL18086923M - OL15423278M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Demonstration of separation delay with glow-discharge plasma actuators
By Lennart S. Hultgren
“Demonstration of separation delay with glow-discharge plasma actuators” Metadata:
- Title: ➤ Demonstration of separation delay with glow-discharge plasma actuators
- Author: Lennart S. Hultgren
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Glenn Research Center - Available from the NASA Center for Aerospace Information
- Publish Date: 2003
- Publish Location: ➤ Hanover, Md - [Cleveland, Ohio] - Springfield, VA
“Demonstration of separation delay with glow-discharge plasma actuators” Subjects and Themes:
- Subjects: Actuators - Flow distribution - Separated flow - Boundary layer separation - Active control
Edition Identifiers:
- The Open Library ID: OL16094111M - OL17635030M
- Online Computer Library Center (OCLC) ID: 56838720
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
By Euromech Colloquium (349th 1996 Göttingen, Germany)
“Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Metadata:
- Title: ➤ Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
- Author: ➤ Euromech Colloquium (349th 1996 Göttingen, Germany)
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Subjects and Themes:
- Subjects: ➤ Airfoil oscillations - Airfoils - Boundary layer separation - Computational fluid dynamics - Coupling - Mach number - Separated flow - Transonic flow - Transonic flutter - Transonic speed - Unsteady flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL17595884M - OL15518388M
- Online Computer Library Center (OCLC) ID: 42671384
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Flow separation in shock wave boundary layer interactions at hypersonic speeds
By A. Hamed
“Flow separation in shock wave boundary layer interactions at hypersonic speeds” Metadata:
- Title: ➤ Flow separation in shock wave boundary layer interactions at hypersonic speeds
- Author: A. Hamed
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Flow separation in shock wave boundary layer interactions at hypersonic speeds” Subjects and Themes:
- Subjects: ➤ Boundary layer separation - Boundary layers - Cylindrical bodies - Flat plates - Hypersonic speed - Oblique shock waves - Shock wave interaction - Turbulent boundary layer
Edition Identifiers:
- The Open Library ID: OL16126865M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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24A study of the factors affecting boundary layer two-dimensionality in wind tunnels
By R. D. Mehta
“A study of the factors affecting boundary layer two-dimensionality in wind tunnels” Metadata:
- Title: ➤ A study of the factors affecting boundary layer two-dimensionality in wind tunnels
- Author: R. D. Mehta
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Stanford University, Dept. of Aeronautics and Astronautics - Joint Institute for Aeronautics and Acoustics
- Publish Date: 1986
- Publish Location: ➤ Stanford, CA - [Springfield, Va
“A study of the factors affecting boundary layer two-dimensionality in wind tunnels” Subjects and Themes:
- Subjects: ➤ Shear stress - Boundary layer separation - Vortices - Mathematical models - Prediction analysis techniques - Aerodynamic configuations - Wings - Fluid mechanics
Edition Identifiers:
- The Open Library ID: OL17684249M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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25Some aspects of aircraft dynamic loads due to flow separation
By D. G. Mabey
“Some aspects of aircraft dynamic loads due to flow separation” Metadata:
- Title: ➤ Some aspects of aircraft dynamic loads due to flow separation
- Author: D. G. Mabey
- Number of Pages: Median: 25
- Publisher: AGARD
- Publish Date: 1988
- Publish Location: Neuilly sur Seine, France
“Some aspects of aircraft dynamic loads due to flow separation” Subjects and Themes:
- Subjects: Aerodynamic loads - Buffeting - Boundary layer separation
Edition Identifiers:
- The Open Library ID: OL20898653M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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26Numerical approach for the aerodynamic analysis of airfoils with laminar separation
By David W. Halt
“Numerical approach for the aerodynamic analysis of airfoils with laminar separation” Metadata:
- Title: ➤ Numerical approach for the aerodynamic analysis of airfoils with laminar separation
- Author: David W. Halt
- Language: English
- Publisher: ➤ McDonnel Douglas Corporation, McDonnel Aircraft Company - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1985
- Publish Location: St. Louis, Mo - Hampton, Va
“Numerical approach for the aerodynamic analysis of airfoils with laminar separation” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerofoils - Airfoils - Boundary layer separation - Computational fluid dynamics - Flow equations - Laminar boundary layer - Laminar flow - Panel method (Fluid dynamics) - Potential flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL16154838M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Simulation of glancing shock wave and boundary layer interaction
By Ching-Mao Hung
“Simulation of glancing shock wave and boundary layer interaction” Metadata:
- Title: ➤ Simulation of glancing shock wave and boundary layer interaction
- Author: Ching-Mao Hung
- Language: English
- Number of Pages: Median: 10
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1989
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Simulation of glancing shock wave and boundary layer interaction” Subjects and Themes:
- Subjects: ➤ Shock waves - Computational fluid dynamics - Computerized simulation - Boundary layer separation - Mathematical models - Fins - Three dimensional flow - Laminar boundary layer
Edition Identifiers:
- The Open Library ID: OL16140340M
Author's Alternative Names:
"Ching-mao Hung"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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28Experimental parametric study of jet vortex generators for flow separation control
By Gregory V. Selby
“Experimental parametric study of jet vortex generators for flow separation control” Metadata:
- Title: ➤ Experimental parametric study of jet vortex generators for flow separation control
- Author: Gregory V. Selby
- Language: English
- Publisher: ➤ Old Dominion University Research Foundation
- Publish Date: 1991
- Publish Location: Norfolk, Va
“Experimental parametric study of jet vortex generators for flow separation control” Subjects and Themes:
- Subjects: ➤ Vortex generators - Turbulent flow - Wind tunnels - Separated flow - Boundary layer separation - Jet flow - Ramps (Structures) - Wind tunnel tests - Boundary layer control - Flow visualization
Edition Identifiers:
- The Open Library ID: OL16131156M
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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29Jet vortex generators for turbulent flow separation control
By Gregory V. Selby
“Jet vortex generators for turbulent flow separation control” Metadata:
- Title: ➤ Jet vortex generators for turbulent flow separation control
- Author: Gregory V. Selby
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - Old Dominion University Research Foundation - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - Hampton, Va - Norfolk, Va
“Jet vortex generators for turbulent flow separation control” Subjects and Themes:
- Subjects: ➤ Vortex generators - Boundary layer control - Boundary layer separation - Jet flow - Free flow - Flow distribution
Edition Identifiers:
- The Open Library ID: OL16129968M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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30Implementation and validation of the Chien k-[epsilon] turbulence model in the Wind Navier-Stokes code
By Dennis A. Yoder
“Implementation and validation of the Chien k-[epsilon] turbulence model in the Wind Navier-Stokes code” Metadata:
- Title: ➤ Implementation and validation of the Chien k-[epsilon] turbulence model in the Wind Navier-Stokes code
- Author: Dennis A. Yoder
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Implementation and validation of the Chien k-[epsilon] turbulence model in the Wind Navier-Stokes code” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Boundary layer separation - K-epsilon turbulence model - Mathematical models - Turbulence models - Incompressible flow - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15550608M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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31Experimental study of saddle point of attachment in laminar juncture flow
By Michael D. Coon
“Experimental study of saddle point of attachment in laminar juncture flow” Metadata:
- Title: ➤ Experimental study of saddle point of attachment in laminar juncture flow
- Author: Michael D. Coon
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics, Inc. - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Washington, DC - [Springfield, Va
“Experimental study of saddle point of attachment in laminar juncture flow” Subjects and Themes:
- Subjects: ➤ Saddle points - Boundary layer separation - Reynolds number - Flow characteristics - Horseshoe vortices - Reattached flow - Flow visualization - Boundary layer transition - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15541834M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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32Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle
By Scott C. Asbury
“Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle” Metadata:
- Title: ➤ Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle
- Author: Scott C. Asbury
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle” Subjects and Themes:
- Subjects: ➤ Wind tunnel nozzles - Oblique shock waves - Flow visualization - Boundary layer separation - Nozzle flow - Wind tunnel tests - Convergent-divergent nozzles
Edition Identifiers:
- The Open Library ID: OL15548828M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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33Final report on study of organized structures in the post-stall flow over wings
By Steven Yon
“Final report on study of organized structures in the post-stall flow over wings” Metadata:
- Title: ➤ Final report on study of organized structures in the post-stall flow over wings
- Author: Steven Yon
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Final report on study of organized structures in the post-stall flow over wings” Subjects and Themes:
- Subjects: ➤ Time dependence - Separated flow - Boundary layer separation - Pressure measurement - Wind tunnels - Frequencies - Angle of attack - Airfoils - Unswept wings - Wakes - Pressure oscillations
Edition Identifiers:
- The Open Library ID: OL15491535M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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34Analysis of aerospike plume induced base-heating environment
By T.-S Wang
“Analysis of aerospike plume induced base-heating environment” Metadata:
- Title: ➤ Analysis of aerospike plume induced base-heating environment
- Author: T.-S Wang
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC - Reston, VA
“Analysis of aerospike plume induced base-heating environment” Subjects and Themes:
- Subjects: ➤ Heat transfer - Convective heat transfer - Base heating - Gray gas - Three dimensional flow - X-33 reusable launch vehicle - Plumes - Aerospike engines - Boundary layer separation - Separated flow
Edition Identifiers:
- The Open Library ID: OL15546870M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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35Some observations on transitory stall in conical diffusers
By K. B. M. Q. Zaman
“Some observations on transitory stall in conical diffusers” Metadata:
- Title: ➤ Some observations on transitory stall in conical diffusers
- Author: K. B. M. Q. Zaman
- Language: English
- Publisher: Lewis Research Center
- Publish Date: 1989
- Publish Location: Cleveland, Ohio
“Some observations on transitory stall in conical diffusers” Subjects and Themes:
- Subjects: Aerodynamic stalling - Conical flow - Diffusion - Boundary layer separation - Pressure recovery
Edition Identifiers:
- The Open Library ID: OL16122156M
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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36Effect of acoustic excitation on stalled flows over an airfoil
By K. B. M. O. Zaman
“Effect of acoustic excitation on stalled flows over an airfoil” Metadata:
- Title: ➤ Effect of acoustic excitation on stalled flows over an airfoil
- Author: K. B. M. O. Zaman
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Effect of acoustic excitation on stalled flows over an airfoil” Subjects and Themes:
- Subjects: Aerodynamic stalling - Acoustic excitation - Airfoil profiles - Boundary layer separation - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15405867M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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37On the Lagrangian description of unsteady boundary layer separation
By Leon L. Van Dommelen
“On the Lagrangian description of unsteady boundary layer separation” Metadata:
- Title: ➤ On the Lagrangian description of unsteady boundary layer separation
- Author: Leon L. Van Dommelen
- Number of Pages: Median: 24
- Publisher: ➤ Institute for Computational Mechanics in Propulsion
- Publish Date: 1989
- Publish Location: Cleveland, Ohio
“On the Lagrangian description of unsteady boundary layer separation” Subjects and Themes:
- Subjects: Unsteady flow - Boundary layer separation
Edition Identifiers:
- The Open Library ID: OL19379479M
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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38On the Lagrangian description of unsteady boundary layer separation
By Leon Van Dommelen
“On the Lagrangian description of unsteady boundary layer separation” Metadata:
- Title: ➤ On the Lagrangian description of unsteady boundary layer separation
- Author: Leon Van Dommelen
- Number of Pages: Median: 48
- Publisher: ➤ Institute for Computational Mechanics in Propulsion
- Publish Date: 1989
- Publish Location: Cleveland, Ohio
“On the Lagrangian description of unsteady boundary layer separation” Subjects and Themes:
- Subjects: Unsteady flow - Boundary layer separation
Edition Identifiers:
- The Open Library ID: OL19379531M
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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39Viscous flow around wall mounted obstacles
By W. H. Schofield
“Viscous flow around wall mounted obstacles” Metadata:
- Title: ➤ Viscous flow around wall mounted obstacles
- Author: W. H. Schofield
- Number of Pages: Median: 28
- Publisher: ➤ Aeronautical Research Laboratories
- Publish Date: 1986
- Publish Location: Melbourne, Australia
“Viscous flow around wall mounted obstacles” Subjects and Themes:
- Subjects: Turbulent flow - Turbulent boundary layer - Pipe flow - Boundary layer separation
Edition Identifiers:
- The Open Library ID: OL19000497M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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