Explore: Potential Flow
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Discrete-vortex model for the symmetric-vortex flow on cones
By Thomas G. Gainer
“Discrete-vortex model for the symmetric-vortex flow on cones” Metadata:
- Title: ➤ Discrete-vortex model for the symmetric-vortex flow on cones
- Author: Thomas G. Gainer
- Language: English
- Number of Pages: Median: 26
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service] - Langley Research Center
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - Washington, D.C - Hampton, Va
“Discrete-vortex model for the symmetric-vortex flow on cones” Subjects and Themes:
- Subjects: ➤ Mathematical models - Vortices - Vortex-motion - Aerodynamics - Flow distribution - Cone - Conical bodies - Potential flow - Cones
Edition Identifiers:
- The Open Library ID: OL16131134M - OL20650553M - OL18246796M - OL21041771M
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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2Small-amplitude disturbances in turbomachine flows with swirl
By David W. Wundrow
“Small-amplitude disturbances in turbomachine flows with swirl” Metadata:
- Title: ➤ Small-amplitude disturbances in turbomachine flows with swirl
- Author: David W. Wundrow
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Small-amplitude disturbances in turbomachine flows with swirl” Subjects and Themes:
- Subjects: ➤ Cascade flow - Compressible flow - Fluid dynamics - Perturbation theory - Potential flow - Steady flow - Swirling - Turbomachine blades
Edition Identifiers:
- The Open Library ID: OL18078606M - OL17005209M - OL15408525M
- Online Computer Library Center (OCLC) ID: 32668514
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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3Delta wings with shock-free cross flow
By S. S. Sritharan
“Delta wings with shock-free cross flow” Metadata:
- Title: ➤ Delta wings with shock-free cross flow
- Author: S. S. Sritharan
- Language: English
- Publisher: ➤ institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1984
- Publish Location: Hampton, Va
“Delta wings with shock-free cross flow” Subjects and Themes:
- Subjects: ➤ Airplanes - Camber - Cross flow - Cross-flow (Aerodynamics) - Delta wings - Potential flow - Shock waves - Supersonic airfoils - Triangular Wings
Edition Identifiers:
- The Open Library ID: OL16154912M - OL18293404M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Extension of transonic flow computational concepts in the analysis of cavitated bearings
By D. Vijayaraghavan
“Extension of transonic flow computational concepts in the analysis of cavitated bearings” Metadata:
- Title: ➤ Extension of transonic flow computational concepts in the analysis of cavitated bearings
- Author: D. Vijayaraghavan
- Language: English
- Publisher: Lewis Research Center
- Publish Date: 1990
- Publish Location: [Cleveland, Ohio
“Extension of transonic flow computational concepts in the analysis of cavitated bearings” Subjects and Themes:
- Subjects: ➤ Analogies - Bearings - Cavitation flow - Computational fluid dynamics - Fluid films - Potential flow - Transonic flow
Edition Identifiers:
- The Open Library ID: OL17725178M - OL17634495M
- Online Computer Library Center (OCLC) ID: 60362126
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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5Potential flow around two-dimensional airfoils using a singular integral method
By Yves Nguyen
“Potential flow around two-dimensional airfoils using a singular integral method” Metadata:
- Title: ➤ Potential flow around two-dimensional airfoils using a singular integral method
- Author: Yves Nguyen
- Language: English
- Number of Pages: Median: 99
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - Fluid Dynamics Group, Bureau of Engineering Research, University of Texas at Austin
- Publish Date: 1987
- Publish Location: ➤ [Washington, D.C - Springfield, Va - Austin, TX
“Potential flow around two-dimensional airfoils using a singular integral method” Subjects and Themes:
- Subjects: ➤ Aerofoils - Singular integrals - Fluid mechanics - Two dimensional bodies - Airfoils - Potential flow - Singular integral equations
Edition Identifiers:
- The Open Library ID: OL14980155M - OL17683676M
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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6A novel potential viscous flow coupling technique for computing helicopter flow fields
By J. Michael Summa
“A novel potential viscous flow coupling technique for computing helicopter flow fields” Metadata:
- Title: ➤ A novel potential viscous flow coupling technique for computing helicopter flow fields
- Author: J. Michael Summa
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1990
- Publish Location: Moffett Field, Calif
“A novel potential viscous flow coupling technique for computing helicopter flow fields” Subjects and Themes:
- Subjects: ➤ Aerodynamic drag - Computational fluid dynamics - Feedback control - Flow distribution - Helicopters - Iteration - Potential flow - Rotary wings - Rotors - Velocity coupling - Velocity distribution
Edition Identifiers:
- The Open Library ID: OL17631923M - OL17725830M
- Online Computer Library Center (OCLC) ID: 63905506
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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7Experimental 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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8Development of direct-inverse 3-D method for applied aerodynamic design and analysis
By Leland A. Carlson
“Development of direct-inverse 3-D method for applied aerodynamic design and analysis” Metadata:
- Title: ➤ Development of direct-inverse 3-D method for applied aerodynamic design and analysis
- Author: Leland A. Carlson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University
- Publish Date: 1987
- Publish Location: ➤ College Station, Tex - Springfield, Va - [Washington, DC
“Development of direct-inverse 3-D method for applied aerodynamic design and analysis” Subjects and Themes:
- Subjects: ➤ Flow equations - Body-wing configurations - Aerodynamics - Coordinates - Design analysis - Transonic flight - Trailing edges - Computer aided design - Aircraft design - Potential flow - Wings
Edition Identifiers:
- The Open Library ID: OL15412083M - OL18080134M
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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9Numerical solution of the full potential equation using a chimera grid approach
By Terry L. Holst
“Numerical solution of the full potential equation using a chimera grid approach” Metadata:
- Title: ➤ Numerical solution of the full potential equation using a chimera grid approach
- Author: Terry L. Holst
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Numerical solution of the full potential equation using a chimera grid approach” Subjects and Themes:
- Subjects: Computational fluid dynamics - Grid generation (Mathematics) - Potential flow - Multiblock grids - Two dimensional flow
Edition Identifiers:
- The Open Library ID: OL17791968M - OL15414553M
- Online Computer Library Center (OCLC) ID: 34072753
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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10On approximate factorization schemes for solving the full potential equation
By Terry L. Holst
“On approximate factorization schemes for solving the full potential equation” Metadata:
- Title: ➤ On approximate factorization schemes for solving the full potential equation
- Author: Terry L. Holst
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Washington, DC
“On approximate factorization schemes for solving the full potential equation” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Iterative solution - Computational grids - Transonic flow - Potential flow - Wings - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15484324M - OL17815469M
- Online Computer Library Center (OCLC) ID: 38067532
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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11Correction for wall-interference by means of a measured-boundary-conditon method
By Th. E. Labrujere
“Correction for wall-interference by means of a measured-boundary-conditon method” Metadata:
- Title: ➤ Correction for wall-interference by means of a measured-boundary-conditon method
- Author: Th. E. Labrujere
- Number of Pages: Median: 41
- Publisher: National Aerospace Laboratory
- Publish Date: 1984
- Publish Location: Amsterdam
“Correction for wall-interference by means of a measured-boundary-conditon method” Subjects and Themes:
- Subjects: ➤ Subsonic flow - Green's functions - Two dimensional flow - Wind tunnel walls - Three dimensional flow - Potential flow
Edition Identifiers:
- The Open Library ID: OL20982753M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Trailing edge flow conditions as a factor in airfoil design
By A. I. Ormsbee
“Trailing edge flow conditions as a factor in airfoil design” Metadata:
- Title: ➤ Trailing edge flow conditions as a factor in airfoil design
- Author: A. I. Ormsbee
- Language: English
- Publisher: ➤ Aeronautical and Astronautical Engineering Dept., University of Illinois - National Aeronautics and Space Administration
- Publish Date: 1984
- Publish Location: Urbana, Ill - [Washington, DC
“Trailing edge flow conditions as a factor in airfoil design” Subjects and Themes:
- Subjects: ➤ Pressure gradients - Trailing edges (Aerodynamics) - Design and construction - Trailing edges - Airfoils - Aircraft design - Potential flow - Aerofoils
Edition Identifiers:
- The Open Library ID: OL16153716M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Study of the mutual interaction between a wing wake and an encountering airplane
By A. B. Walden
“Study of the mutual interaction between a wing wake and an encountering airplane” Metadata:
- Title: ➤ Study of the mutual interaction between a wing wake and an encountering airplane
- Author: A. B. Walden
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Study of the mutual interaction between a wing wake and an encountering airplane” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Panel method (Fluid dynamics) - Configuration interaction - Body-wing configurations - Wakes - Vortices - Potential flow
Edition Identifiers:
- The Open Library ID: OL17132342M
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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14Numerical 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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15Contraction design for small low-speed wind tunnels
By J. H. Bell
“Contraction design for small low-speed wind tunnels” Metadata:
- Title: ➤ Contraction design for small low-speed wind tunnels
- Author: J. H. Bell
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1988
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Contraction design for small low-speed wind tunnels” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Wind tunnel tests - Three dimensional models - Prediction analysis techniques - Two dimensional models - Potential flow - Contraction
Edition Identifiers:
- The Open Library ID: OL15406533M
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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16Control theory based airfoil design for potential flow and a finite volume discretization
By James Reuther
“Control theory based airfoil design for potential flow and a finite volume discretization” Metadata:
- Title: ➤ Control theory based airfoil design for potential flow and a finite volume discretization
- Author: James Reuther
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Control theory based airfoil design for potential flow and a finite volume discretization” Subjects and Themes:
- Subjects: ➤ Three dimensional flow - Finite volume method - Design analysis - Control theory - Optimization - Airfoil profiles - Airfoils - Potential flow
Edition Identifiers:
- The Open Library ID: OL15425936M
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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17A finite volume method for transonic potential flow calculations
By Antony Jameson
“A finite volume method for transonic potential flow calculations” Metadata:
- Title: ➤ A finite volume method for transonic potential flow calculations
- Author: Antony Jameson
- Number of Pages: Median: 54
- Publisher: AIAA
- Publish Date: 1977
- Publish Location: New York
“A finite volume method for transonic potential flow calculations” Subjects and Themes:
- Subjects: Finite volume method - Potential flow - Transonic flow
Edition Identifiers:
- The Open Library ID: OL19380462M
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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18Theory of unsteady compressible irrotational flows including heat conductivity and longitudinal viscosity
By George S. Dulikravich
“Theory of unsteady compressible irrotational flows including heat conductivity and longitudinal viscosity” Metadata:
- Title: ➤ Theory of unsteady compressible irrotational flows including heat conductivity and longitudinal viscosity
- Author: George S. Dulikravich
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1988
- Publish Location: New York
“Theory of unsteady compressible irrotational flows including heat conductivity and longitudinal viscosity” Subjects and Themes:
- Subjects: Potential flow - Unsteady flow - Compressible flow
Edition Identifiers:
- The Open Library ID: OL19380434M
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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19Unsteady potential flow past a propeller blade section
By M. A. Takallu
“Unsteady potential flow past a propeller blade section” Metadata:
- Title: ➤ Unsteady potential flow past a propeller blade section
- Author: M. A. Takallu
- Number of Pages: Median: 25
- Publisher: Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Unsteady potential flow past a propeller blade section” Subjects and Themes:
- Subjects: Potential flow - Propeller blades
Edition Identifiers:
- The Open Library ID: OL21333167M
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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20Control theory based airfoil design using the Euler equations
By Antony Jameson
“Control theory based airfoil design using the Euler equations” Metadata:
- Title: ➤ Control theory based airfoil design using the Euler equations
- Author: Antony Jameson
- Language: English
- Publisher: ➤ Research Institute for Advanced Computer Science, NASA Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Moffett Field, Calif.] - [Springfield, Va
“Control theory based airfoil design using the Euler equations” Subjects and Themes:
- Subjects: ➤ Control theory - Drag - Flow equations - Airfoils - Potential flow - Euler equations of motions - Finite volume method
Edition Identifiers:
- The Open Library ID: OL15403746M
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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21Aerodynamics and heat transfer investigations on a high Reynolds number turbine cascade
By T. Schobeiri
“Aerodynamics and heat transfer investigations on a high Reynolds number turbine cascade” Metadata:
- Title: ➤ Aerodynamics and heat transfer investigations on a high Reynolds number turbine cascade
- Author: T. Schobeiri
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - NASA
- Publish Date: 1991
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Aerodynamics and heat transfer investigations on a high Reynolds number turbine cascade” Subjects and Themes:
- Subjects: ➤ Heat transfer - Boundary layers - Pressure distribution - Aerodynamics - High Reynolds number - Turbines - Temperature effects - Space shuttle main engine - Cascade flow - Potential flow
Edition Identifiers:
- The Open Library ID: OL15405669M
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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22Application of a linearized unsteady aerodynamic analysis to standard cascade configurations
By Joseph M. Verdon
“Application of a linearized unsteady aerodynamic analysis to standard cascade configurations” Metadata:
- Title: ➤ Application of a linearized unsteady aerodynamic analysis to standard cascade configurations
- Author: Joseph M. Verdon
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Application of a linearized unsteady aerodynamic analysis to standard cascade configurations” Subjects and Themes:
- Subjects: ➤ Unsteady flow (Aerodynamics) - Unsteady flow - Unsteady aerodynamics - Cascades (Fluid dynamics) - Aerodynamics - Linearization - Cascade flow - Blades - Potential flow - Flutter - Turbomachines
Edition Identifiers:
- The Open Library ID: OL16116686M
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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23Potential flow downstream of the heliospheric terminal schock
By Steven Nerney
“Potential flow downstream of the heliospheric terminal schock” Metadata:
- Title: ➤ Potential flow downstream of the heliospheric terminal schock
- Author: Steven Nerney
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ Washington, DC - [Springfield, Va
“Potential flow downstream of the heliospheric terminal schock” Subjects and Themes:
- Subjects: Supersonic flow - Heliosphere - Potential flow - Solar wind - Shock waves
Edition Identifiers:
- The Open Library ID: OL15411177M
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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24Potential flow downstream of the heliospheric terminal shock
By Steven Nerney
“Potential flow downstream of the heliospheric terminal shock” Metadata:
- Title: ➤ Potential flow downstream of the heliospheric terminal shock
- Author: Steven Nerney
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Potential flow downstream of the heliospheric terminal shock” Subjects and Themes:
- Subjects: Heliosphere - Potential flow - Solar wind - Shock waves
Edition Identifiers:
- The Open Library ID: OL15498434M
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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Downloads Are Not Available:
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25A numerical analysis applied to high angle of attack three-dimensional inlets
By Danny P. Hwang
“A numerical analysis applied to high angle of attack three-dimensional inlets” Metadata:
- Title: ➤ A numerical analysis applied to high angle of attack three-dimensional inlets
- Author: Danny P. Hwang
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“A numerical analysis applied to high angle of attack three-dimensional inlets” Subjects and Themes:
- Subjects: ➤ Angle of attack - Angle of attack (Aerodynamics) - Computational fluid dynamics - Engine inlets - Fluid dynamics - Inlet flow - Panel method (Fluid dynamics) - Potential flow - Separated flow
Edition Identifiers:
- The Open Library ID: OL16151159M
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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26USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics
By Michael R. Wiese
“USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics” Metadata:
- Title: ➤ USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics
- Author: Michael R. Wiese
- Language: English
- Number of Pages: Median: 97
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: [Washington, D.C.]
“USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics” Subjects and Themes:
- Subjects: ➤ Panel method (Fluid dynamics) - Pressure distribution - Aerodynamics - Supersonic flow - Subsonic flow - Aerodynamic characteristics - Computer programs - Potential flow
Edition Identifiers:
- The Open Library ID: OL16122026M
Access and General Info:
- First Year Published: 1986
- 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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27Unsteady potential flow past a propeller blade section
By Mohammad Ali Takallu
“Unsteady potential flow past a propeller blade section” Metadata:
- Title: ➤ Unsteady potential flow past a propeller blade section
- Author: Mohammad Ali Takallu
- Language: English
- Number of Pages: Median: 25
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1990
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Unsteady potential flow past a propeller blade section” Subjects and Themes:
- Subjects: ➤ Aerial Propellers - Flow distribution - Lift - Potential flow - Pressure distribution - Propeller blades - Propellers, Aerial - Unsteady flow - Unsteady flow (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL16131163M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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28An application of conformal mappings to general grid generation and potential flow problems
By T. R. Bewley
“An application of conformal mappings to general grid generation and potential flow problems” Metadata:
- Title: ➤ An application of conformal mappings to general grid generation and potential flow problems
- Author: T. R. Bewley
- Number of Pages: Median: 16
- Publisher: ➤ von Karman Institute for Fluid Dynamics
- Publish Date: 1990
- Publish Location: Rhode Saint Genese, Belgium
“An application of conformal mappings to general grid generation and potential flow problems” Subjects and Themes:
- Subjects: Potential flow - Grid generation - Conformal mapping
Edition Identifiers:
- The Open Library ID: OL21499351M
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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29ARSPNSC
By M. H. L. Hounjet
“ARSPNSC” Metadata:
- Title: ARSPNSC
- Author: M. H. L. Hounjet
- Number of Pages: Median: 21
- Publisher: National Aerospace Laboratory
- Publish Date: 1986
- Publish Location: Amsterdam
“ARSPNSC” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Wakes - Suction - Wind oscillations - Potential flow - Panel methods (Fluid dynamics)
Edition Identifiers:
- The Open Library ID: OL19252269M
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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30Combining comparison functions and finite element approximations in CFD
By Kenneth J. Baumeister
“Combining comparison functions and finite element approximations in CFD” Metadata:
- Title: ➤ Combining comparison functions and finite element approximations in CFD
- Author: Kenneth J. Baumeister
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Combining comparison functions and finite element approximations in CFD” Subjects and Themes:
- Subjects: Computational fluid dynamics - Finite element method - Potential flow
Edition Identifiers:
- The Open Library ID: OL15411036M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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