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Source: The Open Library
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Search results from The Open Library
1Numerical simulation of the SOFIA flowfield
By Stephen P. Klotz
“Numerical simulation of the SOFIA flowfield” Metadata:
- Title: ➤ Numerical simulation of the SOFIA flowfield
- Author: Stephen P. Klotz
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - San Jose, CA
“Numerical simulation of the SOFIA flowfield” Subjects and Themes:
- Subjects: ➤ Active control - Aerodynamic stalling - Airfoils - Boeing 747 aircraft - Boundary layer control - Cavities - Flow distribution - Leading edges - SOFIA (Airborne observatory) - Separated flow - Sound pressure - Tail assemblies - Telescopes - Unsteady flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17788523M - OL17791647M - OL18081185M - OL18078541M - OL17683431M
- Online Computer Library Center (OCLC) ID: 33433883 - 32647393
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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2In-flight flow visualization results from the X-29A aircraft at high angles of attack
By John H. Del Frate
“In-flight flow visualization results from the X-29A aircraft at high angles of attack” Metadata:
- Title: ➤ In-flight flow visualization results from the X-29A aircraft at high angles of attack
- Author: John H. Del Frate
- Language: English
- Number of Pages: Median: 14
- Publisher: ➤ Dryden Flight Research Facility - For sale by the National Technical Information Service - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ [Washington, DC - Edwards, Calif - Springfield, Va
“In-flight flow visualization results from the X-29A aircraft at high angles of attack” Subjects and Themes:
- Subjects: Flow visualization - Airplanes - Flight testing - Separated flow - X-29 aircraft
Edition Identifiers:
- The Open Library ID: OL15367750M - OL17107179M - OL19247054M - OL18055959M - OL14686366M
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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3Implementation of a two-equation K-[omega] turbulence model in NPARC
By Dennis A. Yoder
“Implementation of a two-equation K-[omega] turbulence model in NPARC” Metadata:
- Title: ➤ Implementation of a two-equation K-[omega] turbulence model in NPARC
- Author: Dennis A. Yoder
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Implementation of a two-equation K-[omega] turbulence model in NPARC” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent boundary layer - Separated flow - Incompressible flow - Turbulence models - Subsonic flow - Boundary layer flow - Applications programs (Computers) - Transition flow - Transistion flow
Edition Identifiers:
- The Open Library ID: OL15423264M - OL18086918M - OL17117628M - OL17117429M
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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4Control 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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5Navier-Stokes analysis of turbine blade heat transfer
By Robert J. Boyle
“Navier-Stokes analysis of turbine blade heat transfer” Metadata:
- Title: ➤ Navier-Stokes analysis of turbine blade heat transfer
- Author: Robert J. Boyle
- Language: English
- Number of Pages: Median: 19
- Publisher: ➤ NASA - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Navier-Stokes analysis of turbine blade heat transfer” Subjects and Themes:
- Subjects: ➤ Aerothermodynamics - Blades - Heat - Heat transfer - Navier-Stokes equation - Reynolds number - Separated flow - Transmission - Turbine blades - Turbines - Vanes
Edition Identifiers:
- The Open Library ID: OL18251832M - OL17630426M - OL16132959M - OL20572886M
- Online Computer Library Center (OCLC) ID: 25311495
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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6Control 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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7Stability of a non-orthagonal stagnation flow to three dimensional disturbances
By D. G. Lasseigne
“Stability of a non-orthagonal stagnation flow to three dimensional disturbances” Metadata:
- Title: ➤ Stability of a non-orthagonal stagnation flow to three dimensional disturbances
- Author: D. G. Lasseigne
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering
- Publish Date: 1991
- Publish Location: Hampton, Va - [Springfield, Va
“Stability of a non-orthagonal stagnation flow to three dimensional disturbances” Subjects and Themes:
- Subjects: ➤ Critical temperature - Flow distribution - Flow stability - Separated flow - Stagnation flow - Stagnation point
Edition Identifiers:
- The Open Library ID: OL16123982M - OL17633054M - OL18226223M
- Online Computer Library Center (OCLC) ID: 59758051
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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8A review of high-speed, convective, heat-transfer computation methods
By Michael E. Tauber
“A review of high-speed, convective, heat-transfer computation methods” Metadata:
- Title: ➤ A review of high-speed, convective, heat-transfer computation methods
- Author: Michael E. Tauber
- Language: English
- Number of Pages: Median: 33
- Publisher: ➤ Ames Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: ➤ Moffett Field, Calif - [Washington, D.C.]
“A review of high-speed, convective, heat-transfer computation methods” Subjects and Themes:
- Subjects: ➤ Aerodynamic heating - Turbulent boundary layer - Convective heat transfer - Separated flow - Transmission - Laminar boundary layer - Heat - Computation - Shock heating
Edition Identifiers:
- The Open Library ID: OL19379677M - OL18225830M - OL16123564M
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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9Unsteady 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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10Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows
By Khaled S. Abdol-Hamid
“Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows” Metadata:
- Title: ➤ Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows
- Author: Khaled S. Abdol-Hamid
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Flow distribution - Flow equations - K-epsilon turbulence model - Navier-Stokes equation - Separated flow - Skin friction
Edition Identifiers:
- The Open Library ID: OL17791165M - OL18080129M - OL15412073M
- Online Computer Library Center (OCLC) ID: 32992169
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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11Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
By Floyd J. Wilcox
“Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6” Metadata:
- Title: ➤ Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
- Author: Floyd J. Wilcox
- Language: English
- Number of Pages: Median: 43
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1995
- Publish Location: ➤ Hampton, Va - Springfield, VA - [Springfield, VA
“Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aerodynamics, Hypersonic - Bombers - Design and construction - External store separation - External stores - Flat plates - Free flow - Hypersonic Aerodynamics - Hypersonic speed - Separated flow
Edition Identifiers:
- The Open Library ID: OL17635043M - OL16125421M - OL17803983M
- Online Computer Library Center (OCLC) ID: 60398151 - 33144596
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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12A computionally efficient modelling of laminar separation bubbles
By Paolo Dini
“A computionally efficient modelling of laminar separation bubbles” Metadata:
- Title: ➤ A computionally efficient modelling of laminar separation bubbles
- Author: Paolo Dini
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Dept. of Aerospace Engineering, Pennsylvania State University
- Publish Date: 1989 - 1990
- Publish Location: ➤ University Park, PA - [Springfield, Va - [Washington, DC
“A computionally efficient modelling of laminar separation bubbles” Subjects and Themes:
- Subjects: ➤ Laminar flow - Computer simulation - Aerofoils - Separated flow - Aerodynamics - Flow characteristics - Prediction analysis techniques - Mathematical models - Bubbles - Airfoils
Edition Identifiers:
- The Open Library ID: OL15396669M - OL15277898M - OL15407502M
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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13Analysis of two-equation turbulence models for recirculating flows
By S. Thangam
“Analysis of two-equation turbulence models for recirculating flows” Metadata:
- Title: ➤ Analysis of two-equation turbulence models for recirculating flows
- Author: S. Thangam
- Language: English
- Number of Pages: Median: 20
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Institute for Computer Applications in Science and Engineering - National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: [Springfield, Va - Hampton, Va
“Analysis of two-equation turbulence models for recirculating flows” Subjects and Themes:
- Subjects: Turbulence - Turbulence models - Backward facing steps - Separated flow - Mathematical models
Edition Identifiers:
- The Open Library ID: OL18066992M - OL21499562M - OL15390846M
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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14In-flight flow visualization characteristics of the NASA F-18 high alpha research vehicle at high angles of attack
By David F. Fisher
“In-flight flow visualization characteristics of the NASA F-18 high alpha research vehicle at high angles of attack” Metadata:
- Title: ➤ In-flight flow visualization characteristics of the NASA F-18 high alpha research vehicle at high angles of attack
- Author: David F. Fisher
- Language: English
- Number of Pages: Median: 31
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Ames Research Center - For sale by the National Technical Information Service]
- Publish Date: 1990 - 1991
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va - [Washington, DC]
“In-flight flow visualization characteristics of the NASA F-18 high alpha research vehicle at high angles of attack” Subjects and Themes:
- Subjects: Flow visualization - Airplanes - F-18 aircraft - Flight testing - Separated flow
Edition Identifiers:
- The Open Library ID: OL15294886M - OL21333277M - OL18033957M
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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15A direct-inverse method for transonic and separated flows about airfoils
By Leland A. Carlson
“A direct-inverse method for transonic and separated flows about airfoils” Metadata:
- Title: ➤ A direct-inverse method for transonic and separated flows about airfoils
- Author: Leland A. Carlson
- Language: English
- Number of Pages: Median: 68
- Publisher: ➤ Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Office
- Publish Date: 1990
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“A direct-inverse method for transonic and separated flows about airfoils” Subjects and Themes:
- Subjects: Aerodynamics - Aerofoils - Transonic flow - Separated flow - Supercritical airfoils
Edition Identifiers:
- The Open Library ID: OL19380405M - OL18030772M - OL15280598M
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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16Enhanced 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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17The structure of separated flow regions occurring near the leading edge of airfoils, including transition
By T. J. Mueller
“The structure of separated flow regions occurring near the leading edge of airfoils, including transition” Metadata:
- Title: ➤ The structure of separated flow regions occurring near the leading edge of airfoils, including transition
- Author: T. J. Mueller
- Language: English
- Publisher: ➤ National Technical Information Service - National Technical Information Service, distributor - Dept. of Aerospace and Mechanical Engineering, University of Notre Dame - National Aeronautics and Space Administration
- Publish Date: 1985 - 1986
- Publish Location: ➤ Notre Dame, Ind - [Springfield, Va - [Washington, D.C - Springfield, Va
“The structure of separated flow regions occurring near the leading edge of airfoils, including transition” Subjects and Themes:
- Subjects: ➤ Aerofoils - Airfoils - Boundary layer transition - Bubbles - Leading edges - Separated flow - Velocity distribution
Edition Identifiers:
- The Open Library ID: OL15416442M - OL15394429M
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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18Application of viscous-inviscid interaction methods to transonic turbulent flows
By D. Lee
“Application of viscous-inviscid interaction methods to transonic turbulent flows” Metadata:
- Title: ➤ Application of viscous-inviscid interaction methods to transonic turbulent flows
- Author: D. Lee
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Engineering Research Institute - National Aeronautics and Space Administration - Iowa State University.
- Publish Date: 1986
- Publish Location: ➤ [Washington, DC - [Ames, Iowa] - Springfield, Va
“Application of viscous-inviscid interaction methods to transonic turbulent flows” Subjects and Themes:
- Subjects: ➤ Axisymmetric bodies - Factorization - Finite difference theory - Iteration - Separated flow - Steady flow - Transonic flow - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL18083416M - OL15417834M
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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19Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight
By John D. Berry
“Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight” Metadata:
- Title: ➤ Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight
- Author: John D. Berry
- Language: English
- Number of Pages: Median: 245
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: Hampton, Va
“Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aerodynamics - Helicopters - Horizontal flight - Rotors (Helicopters) - Separated flow - Testing - Turbulence effects - Unsteady flow - Velocity distribution - Velocity measurment - Wind tunnel tests - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL16137805M - OL17595877M
- Online Computer Library Center (OCLC) ID: 39713178
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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20An investigation of bleed configurations and their effect on shock wave/boundary layer interactions
By A. Hamed
“An investigation of bleed configurations and their effect on shock wave/boundary layer interactions” Metadata:
- Title: ➤ An investigation of bleed configurations and their effect on shock wave/boundary layer interactions
- Author: A. Hamed
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - University of Cincinnati - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Cincinnati, Ohio?] - [Washington, DC
“An investigation of bleed configurations and their effect on shock wave/boundary layer interactions” Subjects and Themes:
- Subjects: ➤ Corner flow - Engine design - Engine inlets - Oblique shock waves - Secondary flow - Separated flow - Shock wave interaction - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL15418954M - OL17793974M
- Online Computer Library Center (OCLC) ID: 34562841
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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21Aircraft dynamic loads due to flow separation
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Aircraft dynamic loads due to flow separation” Metadata:
- Title: ➤ Aircraft dynamic loads due to flow separation
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 272
- Publisher: AGARD
- Publish Date: 1990
- Publish Location: ➤ Neuilly-sur-Seine - Neuilly sur Seine, France
“Aircraft dynamic loads due to flow separation” Subjects and Themes:
- Subjects: ➤ Aerodynamic load - Aerodynamic loads - Aeroelasticity - Buffeting (Aerodynamics) - Congresses - Separated flow
Edition Identifiers:
- The Open Library ID: OL20562784M - OL21334028M
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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22Control 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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23Active control of flow separation over an airfoil
By S. S. Ravindran
“Active control of flow separation over an airfoil” Metadata:
- Title: ➤ Active control of flow separation over an airfoil
- Author: S. S. Ravindran
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Springfield, VA - Hampton, Va
“Active control of flow separation over an airfoil” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Separated flow - Mathematical models - Navier-Stokes equation - Algorithms - Airfoils - Active control - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL17602493M - OL17703416M
- Online Computer Library Center (OCLC) ID: 44140453
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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24Experimental 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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25Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
By John W. Edwards
“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: John W. Edwards
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Flow equations - Unsteady flow - Separated flow - Transonic flow - Transonic flutter - Mach number - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL17838507M - OL15503872M
- Online Computer Library Center (OCLC) ID: 40173648
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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26Demonstration 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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27Numerical simulation of helicopter engine plume in forward flight
By Arsenio C. B. Dimanlig
“Numerical simulation of helicopter engine plume in forward flight” Metadata:
- Title: ➤ Numerical simulation of helicopter engine plume in forward flight
- Author: Arsenio C. B. Dimanlig
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Numerical simulation of helicopter engine plume in forward flight” Subjects and Themes:
- Subjects: ➤ Exhaust gases - Fuselages - Horizontal flight - Flight conditions - Air intakes - Mathematical models - Flow distribution - Helicopter engines - Downwash - Plumes - Rotors - Computerized simulation - Separated flow
Edition Identifiers:
- The Open Library ID: OL17790694M - OL15410201M
- Online Computer Library Center (OCLC) ID: 32834913
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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28Transonic 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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29Study of the unsteady flow features on a stalled wing
By S. Yon
“Study of the unsteady flow features on a stalled wing” Metadata:
- Title: ➤ Study of the unsteady flow features on a stalled wing
- Author: S. Yon
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - Reston, VA - [Washington, DC
“Study of the unsteady flow features on a stalled wing” Subjects and Themes:
- Subjects: ➤ Aerodynamic stalling - Angle of attack - Flow distribution - Frequencies - Rectangular wings - Separated flow - Subsonic wind tunnels - Unsteady flow
Edition Identifiers:
- The Open Library ID: OL15539182M - OL17838077M
- Online Computer Library Center (OCLC) ID: 40832683
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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30Unsteady three-dimensional flow separation
By W. H. Hui
“Unsteady three-dimensional flow separation” Metadata:
- Title: ➤ Unsteady three-dimensional flow separation
- Author: W. H. Hui
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - University of Waterloo Research Institute - National Technical Information Service, distributor
- Publish Date: 1988
- Publish Location: ➤ Waterloo, Ont - Moffett Field, Calif - [Springfield, Va
“Unsteady three-dimensional flow separation” Subjects and Themes:
- Subjects: Aerodynamics - Three dimensional flow - Unsteady flow - Separated flow
Edition Identifiers:
- The Open Library ID: OL18079454M - OL15410366M
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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31Advanced method for computing the flow around wings with rear separation and ground effect
By Klaus Jacob
“Advanced method for computing the flow around wings with rear separation and ground effect” Metadata:
- Title: ➤ Advanced method for computing the flow around wings with rear separation and ground effect
- Author: Klaus Jacob
- Number of Pages: Median: 62
- Publisher: ➤ DFVLR Institut fur Theoretische Stromungsmechanik
- Publish Date: 1986
- Publish Location: Gottingen
“Advanced method for computing the flow around wings with rear separation and ground effect” Subjects and Themes:
- Subjects: Ground effect (Aerodynamics) - Subsonic flow - Separated flow - Wings
Edition Identifiers:
- The Open Library ID: OL19987038M
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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32Advancement of a method for calculating separated flows around airfoils with special consideration of profile drag
By Klaus Jacob
“Advancement of a method for calculating separated flows around airfoils with special consideration of profile drag” Metadata:
- Title: ➤ Advancement of a method for calculating separated flows around airfoils with special consideration of profile drag
- Author: Klaus Jacob
- Number of Pages: Median: 56
- Publisher: European Space Agency
- Publish Date: 1977
- Publish Location: Paris, France
“Advancement of a method for calculating separated flows around airfoils with special consideration of profile drag” Subjects and Themes:
- Subjects: Airfoils - Separated flow
Edition Identifiers:
- The Open Library ID: OL21499317M
Access and General Info:
- First Year Published: 1977
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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33Evaluation of turbulence models for unsteady flows of an oscillating airfoil
By G. R. Srinivasan
“Evaluation of turbulence models for unsteady flows of an oscillating airfoil” Metadata:
- Title: ➤ Evaluation of turbulence models for unsteady flows of an oscillating airfoil
- Author: G. R. Srinivasan
- Language: English
- Publisher: ➤ Pergamon - National Technical Information Service, distributor] - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [New York] - [Washington, D.C - Springfield, Va
“Evaluation of turbulence models for unsteady flows of an oscillating airfoil” Subjects and Themes:
- Subjects: ➤ Aerodynamic stalling - Airfoils - Computational fluid dynamics - Finite difference theory - Flow distribution - Navier-Stokes equation - Oscillations - Separated flow - Turbulence models - Unsteady flow
Edition Identifiers:
- The Open Library ID: OL15504033M
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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34A transport model of the turbulent scalar-velocity
By Ryoichi Amano
“A transport model of the turbulent scalar-velocity” Metadata:
- Title: ➤ A transport model of the turbulent scalar-velocity
- Author: Ryoichi Amano
- Language: English
- Publisher: ➤ Dept. of Mechanical Engineering, University fo Wisconsin--Milwaukee - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1987
- Publish Location: ➤ Springfield, Va - Milwaukee, Wis - [Washington, D.C
“A transport model of the turbulent scalar-velocity” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Separated flow - Prediction analysis techniques - Mathematical models - Turbulence models - Convection - Transport theory
Edition Identifiers:
- The Open Library ID: OL17683845M
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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35Analysis of transitional separation bubbles on infinite swept wings
By R. L. Davis
“Analysis of transitional separation bubbles on infinite swept wings” Metadata:
- Title: ➤ Analysis of transitional separation bubbles on infinite swept wings
- Author: R. L. Davis
- Language: English
- Number of Pages: Median: 35
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Analysis of transitional separation bubbles on infinite swept wings” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Viscous flow - Infinite span wings - Separated flow - Laminar flow - Aerofoils - Boundary layer transition - Bubbles - Boundary layer - Wall flow
Edition Identifiers:
- The Open Library ID: OL16116439M
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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36Control of separated flow past a cylinder using tangential wall jet blowing
By Sejong Oh
“Control of separated flow past a cylinder using tangential wall jet blowing” Metadata:
- Title: ➤ Control of separated flow past a cylinder using tangential wall jet blowing
- Author: Sejong Oh
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Control of separated flow past a cylinder using tangential wall jet blowing” Subjects and Themes:
- Subjects: ➤ Circular cylinders - Fluid dynamics - Separated flow - Airfoils - Pressure gradients - Wall jets - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15409350M
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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37Numerical investigation of the effects of icing on fixed and rotary wing aircraft
By Lakshmi N. Sankar
“Numerical investigation of the effects of icing on fixed and rotary wing aircraft” Metadata:
- Title: ➤ Numerical investigation of the effects of icing on fixed and rotary wing aircraft
- Author: Lakshmi N. Sankar
- Language: English
- Number of Pages: Median: 21
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1992
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Numerical investigation of the effects of icing on fixed and rotary wing aircraft” Subjects and Themes:
- Subjects: ➤ Helicopters - Fixed wings - Computational fluid dynamics - Cold weather operation - Icing (Meteorology) - Rotary wings - Aerodynamic characteristics - Two dimensional models - Aircraft performance - Ice prevention - Three dimensional models - Separated flow - Aircraft icing - Ice formation - Surface roughness - Airplanes - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15410922M
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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38Turbulent separated flow in the vicinity of a single-slotted airfoil flap
By D. Adair
“Turbulent separated flow in the vicinity of a single-slotted airfoil flap” Metadata:
- Title: ➤ Turbulent separated flow in the vicinity of a single-slotted airfoil flap
- Author: D. Adair
- Number of Pages: Median: 13
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1988
- Publish Location: Washington, D. C
“Turbulent separated flow in the vicinity of a single-slotted airfoil flap” Subjects and Themes:
- Subjects: Turbulent flow - Separated flow
Edition Identifiers:
- The Open Library ID: OL19245219M
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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39Attached and separated trailing edge flow measurements with a triple-split hot-film probe
By Michael Donald Doiron
“Attached and separated trailing edge flow measurements with a triple-split hot-film probe” Metadata:
- Title: ➤ Attached and separated trailing edge flow measurements with a triple-split hot-film probe
- Author: Michael Donald Doiron
- Number of Pages: Median: 111
- Publisher: ➤ University of Toronto, Graduate Department of Aerospace Science and Engineering
- Publish Date: 1992
- Publish Location: [Toronto, Ont.]
“Attached and separated trailing edge flow measurements with a triple-split hot-film probe” Subjects and Themes:
- Subjects: Hot-film anemometers - Trailing edges - Separated flow
Edition Identifiers:
- The Open Library ID: OL19246488M
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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40Experimental 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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41Thin layer approximation and algebraic model for separated turbulent flows
By Barrett S. Baldwin
“Thin layer approximation and algebraic model for separated turbulent flows” Metadata:
- Title: ➤ Thin layer approximation and algebraic model for separated turbulent flows
- Author: Barrett S. Baldwin
- Publisher: AIAA
- Publish Date: 1978
- Publish Location: New York
“Thin layer approximation and algebraic model for separated turbulent flows” Subjects and Themes:
- Subjects: Turbulent flow - Separated flow
Edition Identifiers:
- The Open Library ID: OL19000940M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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42Computation of separated and unsteady flows with one- and two-equation turbulence models
By J. A. Ekaterinaris
“Computation of separated and unsteady flows with one- and two-equation turbulence models” Metadata:
- Title: ➤ Computation of separated and unsteady flows with one- and two-equation turbulence models
- Author: J. A. Ekaterinaris
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - Washington, D.C
“Computation of separated and unsteady flows with one- and two-equation turbulence models” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Eddy viscosity - Upwind schemes (Mathematics) - Unsteady flow - Computerized simulation - Turbulence models - Flow distribution - High Reynolds number - Leading edges - Navier-Stokes equation - Transition flow - Separated flow
Edition Identifiers:
- The Open Library ID: OL15501779M
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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43Effect of turbulence models on two massively-separated benchmark flow cases
By C. L. Rumsey
“Effect of turbulence models on two massively-separated benchmark flow cases” Metadata:
- Title: ➤ Effect of turbulence models on two massively-separated benchmark flow cases
- Author: C. L. Rumsey
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2003
- Publish Location: ➤ Hampton, Va - Springfield, VA - Hanover, MD
“Effect of turbulence models on two massively-separated benchmark flow cases” Subjects and Themes:
- Subjects: Computational fluid dynamics - Turbulence models - Separated flow
Edition Identifiers:
- The Open Library ID: OL16116873M
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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44Summary of EASM turbulence models in CFL3D with validation test cases
By C. L. Rumsey
“Summary of EASM turbulence models in CFL3D with validation test cases” Metadata:
- Title: ➤ Summary of EASM turbulence models in CFL3D with validation test cases
- Author: C. L. Rumsey
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2003
- Publish Location: Hampton, Va - Hanover MD
“Summary of EASM turbulence models in CFL3D with validation test cases” Subjects and Themes:
- Subjects: ➤ Coding - Computational fluid dynamics - K-epsilon turbulence model - K-omega turbulence model - Program verification (Computers) - Separated flow - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL16111169M
Access and General Info:
- First Year Published: 2003
- 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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45Enhanced line integral convolution with flow feature detection
By Arthur Okada
“Enhanced line integral convolution with flow feature detection” Metadata:
- Title: ➤ Enhanced line integral convolution with flow feature detection
- Author: Arthur Okada
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Enhanced line integral convolution with flow feature detection” Subjects and Themes:
- Subjects: ➤ Reattached flow - Image enhancement - Separated flow - Flow visualization - Algorithms - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15543353M
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.
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46Turbulence modeling
By Jorge E. Bardina
“Turbulence modeling” Metadata:
- Title: Turbulence modeling
- Author: Jorge E. Bardina
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Turbulence modeling” Subjects and Themes:
- Subjects: ➤ Computerized simulation - Hypersonic flow - Turbulence models - Program verification (Computers) - Navier-Stokes equation - Separated flow - Hypersonic speed - Computer aided design - Computer programs - Compressibility - Transition flow - Hypersonic shock
Edition Identifiers:
- The Open Library ID: OL15413741M
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:
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47Assessment of an unstructured-grid method for predicting 3-D turbulent viscous flows
By Aerospace Sciences Meeting & Exhibit (34th 1996 Reno, Nev.)
“Assessment of an unstructured-grid method for predicting 3-D turbulent viscous flows” Metadata:
- Title: ➤ Assessment of an unstructured-grid method for predicting 3-D turbulent viscous flows
- Author: ➤ Aerospace Sciences Meeting & Exhibit (34th 1996 Reno, Nev.)
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - Washington, D.C
“Assessment of an unstructured-grid method for predicting 3-D turbulent viscous flows” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Three dimensional flow - Unstructured grids (Mathematics) - Separated flow - Turbulence effects
Edition Identifiers:
- The Open Library ID: OL15507931M
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:
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48Final 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
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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49PARC3D calculations of the F/A-18A HARV inlet vortex generators
By Steve D. Podleski
“PARC3D calculations of the F/A-18A HARV inlet vortex generators” Metadata:
- Title: ➤ PARC3D calculations of the F/A-18A HARV inlet vortex generators
- Author: Steve D. Podleski
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“PARC3D calculations of the F/A-18A HARV inlet vortex generators” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Flow distortion - F-18 aircraft - Separated flow - Computational grids - Vortex generators - Applications programs (Computers) - Transonic speed - Engine inlets - Maneuverability - Research vehicles
Edition Identifiers:
- The Open Library ID: OL15425817M
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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50Control of leading-edge separation on an airfoil by localized excitation
By Alexander Dovgal
“Control of leading-edge separation on an airfoil by localized excitation” Metadata:
- Title: ➤ Control of leading-edge separation on an airfoil by localized excitation
- Author: Alexander Dovgal
- Number of Pages: Median: 54
- Publisher: DLR
- Publish Date: 1993
- Publish Location: Koln
“Control of leading-edge separation on an airfoil by localized excitation” Subjects and Themes:
- Subjects: Airfoils - Separated flow
Edition Identifiers:
- The Open Library ID: OL19750728M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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