Explore: *unsteady Aerodynamics
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Source: The Open Library
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Search results from The Open Library
1A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows
By Matthew D. Montgomery
“A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows” Metadata:
- Title: ➤ A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows
- Author: Matthew D. Montgomery
- Language: English
- Number of Pages: Median: 83
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor] - National Technical Information Service, distributor - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1996 - 1997
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va - [Washington, DC]
“A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Mathematical models - Three dimensional models - Unsteady aerodynamics - Three dimensional flow - Aerodynamic characteristics - Boundary conditions - Euler equations of motion - Turbomachine blades - Unsteady flow (Aerodynamics) - Fluid dynamics - Boundary layer - Turbomachines
Edition Identifiers:
- The Open Library ID: ➤ OL18121541M - OL17576345M - OL18121455M - OL18998858M - OL15504972M - OL17576348M - OL17126336M - OL17126578M
- Online Computer Library Center (OCLC) ID: 40238889 - 40154543
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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2Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
By Kenneth W. Iliff
“Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring” Metadata:
- Title: ➤ Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
- Author: Kenneth W. Iliff
- Language: English
- Number of Pages: Median: 65
- Publisher: ➤ National Technical Information Service, distributor - NASA, Dryden Flight Research Center - National Aeronautics and Space Administration, Dryden Flight Research Center - Available from National Technical Information Service
- Publish Date: 1997
- Publish Location: ➤ Edwards, Calif - Springfield, Va - [Springfield, Va
“Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring” Subjects and Themes:
- Subjects: ➤ Aircraft control - Airplanes - Angle of attack - Angle of attack (Aerodynamics) - Control surfaces - Control systems - Flight tests - Hornet (Jet fighter plane) - Longitudinal Stability of airplanes - Longitudinal stability - Maximum likelihood estimates - Parameter identification - Research vehicles - Thrust vector control - Unsteady aerodynamics - Yawing (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL19396278M - OL18134930M - OL17135417M - OL15548785M - OL17591853M
- Online Computer Library Center (OCLC) ID: 42758582
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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3On automating domain connectivity for overset grids
By Ing-Tsau Chiu
“On automating domain connectivity for overset grids” Metadata:
- Title: ➤ On automating domain connectivity for overset grids
- Author: Ing-Tsau Chiu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Overset Methods, Inc. - National Technical Information Service, distributor - OMI
- Publish Date: 1994 - 1995
- Publish Location: ➤ Los Altos, CA - Springfield, Va - Vacaville, CA - [Washington, DC
“On automating domain connectivity for overset grids” Subjects and Themes:
- Subjects: ➤ Cartesian coordinates - Complex systems - Computational fluid dynamics - Computational geometry - Computational grids - Flow distribution - Fluid dynamics - Grid generation (Mathematics) - Multiblock grids - Unsteady aerodynamics - Unsteady flow
Edition Identifiers:
- The Open Library ID: OL17790034M - OL17794003M - OL15400595M - OL15419101M
- Online Computer Library Center (OCLC) ID: 31990521 - 34559246
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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4Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine
By Daniel J. Dorney
“Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine” Metadata:
- Title: ➤ Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine
- Author: Daniel J. Dorney
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine” Subjects and Themes:
- Subjects: ➤ Blade-vortex interaction - Navier-Stokes equation - Propulsive efficiency - Reynolds number - Rotor stator interactions - Turbine blades - Turbines - Unsteady aerodynamics - Unsteady flow - Wakes
Edition Identifiers:
- The Open Library ID: OL17546454M - OL18116215M - OL17123448M - OL15491903M
- Online Computer Library Center (OCLC) ID: 39109525
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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5Three-dimensional Euler time accurate simulations of fan rotor-stator interactions
By A. A. Boretti
“Three-dimensional Euler time accurate simulations of fan rotor-stator interactions” Metadata:
- Title: ➤ Three-dimensional Euler time accurate simulations of fan rotor-stator interactions
- Author: A. A. Boretti
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ Lewis Research Centre - For sale by the National Technical Information Service - National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion
- Publish Date: 1990
- Publish Location: ➤ [Cleveland, Ohio - Cleveland, Ohio - Springfield, Va
“Three-dimensional Euler time accurate simulations of fan rotor-stator interactions” Subjects and Themes:
- Subjects: ➤ Three dimensional flow - Unsteady flow (Aerodynamics) - Unsteady aerodynamics - Turbomachinery - Flow distribution - Euler equations of motion - Rotor stator interactions - Rotor dynamics - Interactional aerodynamics - Stators
Edition Identifiers:
- The Open Library ID: OL19246815M - OL17630435M - OL16124000M - OL18226226M
- Online Computer Library Center (OCLC) ID: 59760034
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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6User's guide for ENSAERO--a multidisciplinary program for fluid/structural/control interaction studies of aircraft (release 1)
By Guru P. Guruswamy
“User's guide for ENSAERO--a multidisciplinary program for fluid/structural/control interaction studies of aircraft (release 1)” Metadata:
- Title: ➤ User's guide for ENSAERO--a multidisciplinary program for fluid/structural/control interaction studies of aircraft (release 1)
- Author: Guru P. Guruswamy
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“User's guide for ENSAERO--a multidisciplinary program for fluid/structural/control interaction studies of aircraft (release 1)” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Computational fluid dynamics - Dynamic structural analysis - Euler equations of motion - Navier-Stokes equation - Unsteady aerodynamics - User manuals (Computer porgrams)
Edition Identifiers:
- The Open Library ID: OL15408173M - OL18078498M - OL17788475M - OL17114583M
- Online Computer Library Center (OCLC) ID: 32638898
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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7Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
By E. Carson Yates
“Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design” Metadata:
- Title: ➤ Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
- Author: E. Carson Yates
- Language: English
- Number of Pages: Median: 15
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va - [Springfield, Va
“Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Inviscid flow - Viscous flow - Integral equations - Unsteady aerodynamics - Transonic flow - Computer aided design - Supersonics
Edition Identifiers:
- The Open Library ID: OL20650523M - OL17630478M - OL16131061M - OL18246750M
- Online Computer Library Center (OCLC) ID: 25058132
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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8Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes
By William L. Kleb
“Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes” Metadata:
- Title: ➤ Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes
- Author: William L. Kleb
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes” Subjects and Themes:
- Subjects: ➤ Grid generation (Mathematics) - Unsteady aerodynamics - Two dimensional flow - Euler equations of motion - Airfoil profiles - Adaptive control - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL18077428M - OL17114326M - OL15406062M
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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9Unsteady blade-surface pressures on a large-scale advanced propeller
By M. Nallasamy
“Unsteady blade-surface pressures on a large-scale advanced propeller” Metadata:
- Title: ➤ Unsteady blade-surface pressures on a large-scale advanced propeller
- Author: M. Nallasamy
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Unsteady blade-surface pressures on a large-scale advanced propeller” Subjects and Themes:
- Subjects: ➤ Unsteady aerodynamics - Prediction analysis techniques - Propeller blade - Pressure oscillations - Elastic waves - Flow distribution
Edition Identifiers:
- The Open Library ID: OL18077396M - OL17114296M - OL15405944M
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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10Estimation of aircraft nonlinear unsteady parameters from wind tunnel data
By Vladislav Klein
“Estimation of aircraft nonlinear unsteady parameters from wind tunnel data” Metadata:
- Title: ➤ Estimation of aircraft nonlinear unsteady parameters from wind tunnel data
- Author: Vladislav Klein
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: Hampton, Va - [Springfield, Va
“Estimation of aircraft nonlinear unsteady parameters from wind tunnel data” Subjects and Themes:
- Subjects: ➤ Aerodynamic forces - Aircraft stability - Flight stability tests - Mathematical models - Unsteady aerodynamics - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17839051M - OL15542530M
- Online Computer Library Center (OCLC) ID: 41469910
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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11Modeling of aircraft unsteady aerodynamic characteristics
By Vladislav Klein
“Modeling of aircraft unsteady aerodynamic characteristics” Metadata:
- Title: ➤ Modeling of aircraft unsteady aerodynamic characteristics
- Author: Vladislav Klein
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994 - 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Modeling of aircraft unsteady aerodynamic characteristics” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Applications programs (Computers) - F-18 aircraft - Stability derivatives - Stability of airplanes - Unsteady aerodynamics - X-31 aircraft
Edition Identifiers:
- The Open Library ID: OL15398601M - OL15498106M
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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12STARS
By Kajal K. Gupta
“STARS” Metadata:
- Title: STARS
- Author: Kajal K. Gupta
- Language: English
- Number of Pages: Median: 160
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - For sale by the National Technical Information Service
- Publish Date: 1990 - 1991
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“STARS” Subjects and Themes:
- Subjects: ➤ Aerodynamic forces - Aeroelasticity - Aeroservoelasticity - Computer programs - Control stability - Finite element method - Structural analysis - Structural analysis (Engineering) - Subsonic flow - Supersonic flow - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL16131038M - OL16132316M
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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13Unsteady aerodynamic phenomena in turbomachines
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Unsteady aerodynamic phenomena in turbomachines” Metadata:
- Title: ➤ Unsteady aerodynamic phenomena in turbomachines
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 323
- Publisher: AGARD
- Publish Date: 1990
- Publish Location: ➤ Neuilly-sur-Seine - Neuilly sur Seine, France
“Unsteady aerodynamic phenomena in turbomachines” Subjects and Themes:
- Subjects: Turbomachinery - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL21333487M - OL20117004M
- All ISBNs: 9283505433 - 9789283505433
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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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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15Active 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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16Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
By Jensen Lin
“Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation” Metadata:
- Title: ➤ Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
- Author: Jensen Lin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 2000
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Aeroelasticity - Laplace transformation - Lift - Method of moments - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL17596830M - OL17704161M
- Online Computer Library Center (OCLC) ID: 45009645
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17Transonic 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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18Indicial response approach derived from Navier-Stokes equations
By K. V. Truong
“Indicial response approach derived from Navier-Stokes equations” Metadata:
- Title: ➤ Indicial response approach derived from Navier-Stokes equations
- Author: K. V. Truong
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Indicial response approach derived from Navier-Stokes equations” Subjects and Themes:
- Subjects: Oscillations - Velocity distribution - Navier-Stokes equation - Unsteady aerodynamics - Vortices
Edition Identifiers:
- The Open Library ID: OL17114226M - OL17683125M
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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19Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques
By Walter A. Silva
“Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques” Metadata:
- Title: ➤ Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques
- Author: Walter A. Silva
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, D.C - Hampton, Va - [Springfield, Va
“Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Unsteady aerodynamics - Navier-Stokes equation - Aeroelasticity - Nonlinear systems - Impulses - Mathematical models - Digital filters - Linear systems
Edition Identifiers:
- The Open Library ID: OL15503907M - OL15543097M
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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20Propulsive performance of two dimensional thin airfoils undergoing large amplitude pitch and plunge oscillations
By James D. Fairgrieve
“Propulsive performance of two dimensional thin airfoils undergoing large amplitude pitch and plunge oscillations” Metadata:
- Title: ➤ Propulsive performance of two dimensional thin airfoils undergoing large amplitude pitch and plunge oscillations
- Author: James D. Fairgrieve
- Publisher: ➤ Dept. of Aerospace Science and Engineering - Institute for Aerospace Studies
- Publish Date: 1979 - 1982
- Publish Location: [Downsview, Ont.]
“Propulsive performance of two dimensional thin airfoils undergoing large amplitude pitch and plunge oscillations” Subjects and Themes:
- Subjects: Oscillating wing aerodynamics - Propulsion - Flapping wing - Unsteady aerodynamics - Airfoils
Edition Identifiers:
- The Open Library ID: OL20968307M - OL19988546M
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Aeroelastic simulation of higher harmonic control
By Lawson H. Robinson
“Aeroelastic simulation of higher harmonic control” Metadata:
- Title: ➤ Aeroelastic simulation of higher harmonic control
- Author: Lawson H. Robinson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1994
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Aeroelastic simulation of higher harmonic control” Subjects and Themes:
- Subjects: ➤ Harmonic control - Unsteady aerodynamics - Helicopter control - Rotor aerodynamics - Rigid rotors - Rotor dynamics - Vibration damping - Aeroelasticity
Edition Identifiers:
- The Open Library ID: OL15403652M - OL17790234M
- Online Computer Library Center (OCLC) ID: 32219948
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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22Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows
By A. A. Boretti
“Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows” Metadata:
- Title: ➤ Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows
- Author: A. A. Boretti
- Language: English
- Number of Pages: Median: 20
- Publisher: ➤ NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ Cleveland, Ohio - [Springfield, Va
“Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows” Subjects and Themes:
- Subjects: ➤ Rotors - Unsteady flow - Computerized simulation - Mathematical models - Navier-Stokes equation - Dynamics - Flow distribution - Runge-Kutta method - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL18087044M - OL15423603M
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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23Development of a linearized unsteady Euler analysis for turbomachinery blade rows
By Joseph M. Verdon
“Development of a linearized unsteady Euler analysis for turbomachinery blade rows” Metadata:
- Title: ➤ Development of a linearized unsteady Euler analysis for turbomachinery blade rows
- Author: Joseph M. Verdon
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Development of a linearized unsteady Euler analysis for turbomachinery blade rows” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Differential equations - Axial flow - Unsteady aerodynamics - Rotor blades (Turbomachinery) - Inviscid flow - Euler equations of motion - Linearization - Surface properties - Three dimensional flow
Edition Identifiers:
- The Open Library ID: OL17792062M - OL15414585M
- Online Computer Library Center (OCLC) ID: 34041808
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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24FPCAS3D user's guide
By Milind A. Bakhle
“FPCAS3D user's guide” Metadata:
- Title: FPCAS3D user's guide
- Author: Milind A. Bakhle
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“FPCAS3D user's guide” Subjects and Themes:
- Subjects: ➤ Unsteady aerodynamics - User manuals (Computer programs) - Flutter analysis - Applications programs (Computers) - Aerodynamic stability - Aeroelasticity - Flutter - Finite element method
Edition Identifiers:
- The Open Library ID: OL15414978M - OL17792146M
- Online Computer Library Center (OCLC) ID: 33973418
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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25Experimental unsteady aerodynamics of conventional and supercritical airfoils
By Sanford S. Davis
“Experimental unsteady aerodynamics of conventional and supercritical airfoils” Metadata:
- Title: ➤ Experimental unsteady aerodynamics of conventional and supercritical airfoils
- Author: Sanford S. Davis
- Number of Pages: Median: 94
- Publisher: Ames Research Center
- Publish Date: 1980
- Publish Location: Moffett Field, Calif
“Experimental unsteady aerodynamics of conventional and supercritical airfoils” Subjects and Themes:
- Subjects: Airfoils - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL19380408M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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26Unsteady aerodynamics of conventional and supercritical airfoils
By Sanford S. Davis
“Unsteady aerodynamics of conventional and supercritical airfoils” Metadata:
- Title: ➤ Unsteady aerodynamics of conventional and supercritical airfoils
- Author: Sanford S. Davis
- Number of Pages: Median: 433
- Publisher: AIAA
- Publish Date: 1980
- Publish Location: New York
“Unsteady aerodynamics of conventional and supercritical airfoils” Subjects and Themes:
- Subjects: Airfoils - Supercritical airfoils - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL19380463M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data
By Vladislav Klein
“Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data” Metadata:
- Title: ➤ Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data
- Author: Vladislav Klein
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Fighter aircraft - Supersonic aircraft - Unsteady aerodynamics - X-29 aircraft - X-31 aircraft
Edition Identifiers:
- The Open Library ID: OL15542100M
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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28Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines
By Om P. Sharma
“Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines” Metadata:
- Title: ➤ Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines
- Author: Om P. Sharma
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Axial flow - Unsteady flow - Unsteady aerodynamics - Turbomachinery - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL17837361M
- Online Computer Library Center (OCLC) ID: 40168805
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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29Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver
By Milind A. Bakhle
“Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver” Metadata:
- Title: ➤ Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver
- Author: Milind A. Bakhle
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver” Subjects and Themes:
- Subjects: ➤ Euler equations of motion - Unsteady aerodynamics - Computer programs - Rotor dynamics - Aeroelasticity - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL17834509M
- Online Computer Library Center (OCLC) ID: 39725973
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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30Revised results of the unsteady transonic pressure measurements on the LANN model
By R. G. den Boer
“Revised results of the unsteady transonic pressure measurements on the LANN model” Metadata:
- Title: ➤ Revised results of the unsteady transonic pressure measurements on the LANN model
- Author: R. G. den Boer
- Number of Pages: Median: 156
- Publisher: National Aerospace Laboratory
- Publish Date: 1989
- Publish Location: Amsterdam
“Revised results of the unsteady transonic pressure measurements on the LANN model” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL21378584M
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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31Modeling of unsteady three-dimensional flows in multistage machines
By Kenneth C. Hall
“Modeling of unsteady three-dimensional flows in multistage machines” Metadata:
- Title: ➤ Modeling of unsteady three-dimensional flows in multistage machines
- Author: Kenneth C. Hall
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2003
- Publish Location: ➤ Hanover, MD - [Cleveland, Ohio]
“Modeling of unsteady three-dimensional flows in multistage machines” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Heat transfer - Three dimensional models - Unsteady flow - Unsteady aerodynamics - Three dimensional flow - Applications programs (Computers) - Turbomachinery
Edition Identifiers:
- The Open Library ID: OL16055682M
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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32A numerical study of fundamental shock noise mechanisms
By Kristine R. Meadows
“A numerical study of fundamental shock noise mechanisms” Metadata:
- Title: ➤ A numerical study of fundamental shock noise mechanisms
- Author: Kristine R. Meadows
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“A numerical study of fundamental shock noise mechanisms” Subjects and Themes:
- Subjects: ➤ Lighthill method - Numerical analysis - Aeroacoustics - Unsteady aerodynamics - Noise prediction - Supersonic jet flow - Jet aircraft noise - Aerodynamic noise - Sound generators - Unsteady flow - Shock wave interaction - Shock wave propagation - Shock waves
Edition Identifiers:
- The Open Library ID: OL15413555M
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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33ASTROP2 users manual
By T. S. R. Reddy
“ASTROP2 users manual” Metadata:
- Title: ASTROP2 users manual
- Author: T. S. R. Reddy
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“ASTROP2 users manual” Subjects and Themes:
- Subjects: ➤ Unsteady aerodynamics - User manuals (Computer programs) - Contrarotating propellers - Finite element method - Computer programs - Aerodynamic forces - Aeroelasticity - Flutter
Edition Identifiers:
- The Open Library ID: OL15496478M
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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34User's guide for ECAP2D
By T. S. R. Reddy
“User's guide for ECAP2D” Metadata:
- Title: User's guide for ECAP2D
- Author: T. S. R. Reddy
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“User's guide for ECAP2D” Subjects and Themes:
- Subjects: ➤ Unsteady aerodynamics - Two dimensional flow - Euler equations of motion - Aeroelasticity - User manuals (Computer programs) - Computer programs - Cascade flow
Edition Identifiers:
- The Open Library ID: OL15411264M
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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35User's guide for MSAP2D
By T. S. R. Reddy
“User's guide for MSAP2D” Metadata:
- Title: User's guide for MSAP2D
- Author: T. S. R. Reddy
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“User's guide for MSAP2D” Subjects and Themes:
- Subjects: ➤ Dynamic response - Unsteady aerodynamics - User manuals (Computer programs) - Rotor blades (Turbomachinery) - Turbocompressors - Computer programs - Aeroelasticity - Flutter
Edition Identifiers:
- The Open Library ID: OL15505221M
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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36Additional development of the XTRAN3S computer program
By Christopher J. Borland
“Additional development of the XTRAN3S computer program” Metadata:
- Title: ➤ Additional development of the XTRAN3S computer program
- Author: Christopher J. Borland
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1989
- Publish Location: Hampton, Va - [Springfield, Va
“Additional development of the XTRAN3S computer program” Subjects and Themes:
- Subjects: ➤ Unsteady aerodynamics - Computer programs - Flutter analysis - Transonic flow - Aeroelasticity - Wing profiles - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15407720M
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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37Structural Dynamics Division research and technology accomplishments for FY 1989 and plans for FY 1990
By Jacqueline G. Smith
“Structural Dynamics Division research and technology accomplishments for FY 1989 and plans for FY 1990” Metadata:
- Title: ➤ Structural Dynamics Division research and technology accomplishments for FY 1989 and plans for FY 1990
- Author: Jacqueline G. Smith
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Structural Dynamics Division research and technology accomplishments for FY 1989 and plans for FY 1990” Subjects and Themes:
- Subjects: Dynamic response - Aeroelasticity - Research and development - Dynamic structural analysis - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL16138588M
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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38Analysis of wind tunnel oscillatory data of the X-31A aircraft
By Mark S. Smith
“Analysis of wind tunnel oscillatory data of the X-31A aircraft” Metadata:
- Title: ➤ Analysis of wind tunnel oscillatory data of the X-31A aircraft
- Author: Mark S. Smith
- 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
“Analysis of wind tunnel oscillatory data of the X-31A aircraft” Subjects and Themes:
- Subjects: ➤ X-31 aircraft - Unsteady aerodynamics - Mathematical models - Wind tunnel tests - Static stability - Scale models - Dynamic stability - Harmonic oscillation - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15542620M
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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39A review of turbomachinery blade-row interaction research
By Todd E. Smith
“A review of turbomachinery blade-row interaction research” Metadata:
- Title: ➤ A review of turbomachinery blade-row interaction research
- Author: Todd E. Smith
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - Lewis Research Center, National Aeronautics and Space Administration
- Publish Date: 1988
- Publish Location: ➤ [Springfield, Va - Cleveland, Ohio
“A review of turbomachinery blade-row interaction research” Subjects and Themes:
- Subjects: Oscillations - Literature - Unsteady aerodynamics - Aerodynamic interference - Turbomachine blades
Edition Identifiers:
- The Open Library ID: OL15407669M
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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40A historical overview of flight flutter testing
By M. W. Kehoe
“A historical overview of flight flutter testing” Metadata:
- Title: ➤ A historical overview of flight flutter testing
- Author: M. W. Kehoe
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“A historical overview of flight flutter testing” Subjects and Themes:
- Subjects: ➤ Aircraft stability - Flutter analysis histories - Excitation - Experiment design - Unsteady aerodynamics - Procedures - Dynamic structural analysis
Edition Identifiers:
- The Open Library ID: OL16125631M
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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41Astrop3 user's guide
By R. August
“Astrop3 user's guide” Metadata:
- Title: Astrop3 user's guide
- Author: R. August
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Astrop3 user's guide” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aeroelasticity - Computer programs - Dynamic analysis - FORTRAN - Prop-fan technology - Propeller fans - Propulsion system configurations - Propulsion system performance - Rotation - Unsteady aerodynamics - User manuals (Computer programs)
Edition Identifiers:
- The Open Library ID: OL15405819M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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42Computational aeroservoelastic analysis with an Euler-based unsteady flow solver
By Andrew S. Arena
“Computational aeroservoelastic analysis with an Euler-based unsteady flow solver” Metadata:
- Title: ➤ Computational aeroservoelastic analysis with an Euler-based unsteady flow solver
- Author: Andrew S. Arena
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Computational aeroservoelastic analysis with an Euler-based unsteady flow solver” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Unsteady flow - Unsteady aerodynamics - Transpiration - Supersonic flow - Aeroservoelasticity - Finite element method - Mach number
Edition Identifiers:
- The Open Library ID: OL15508616M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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43Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack
By M. Nallasamy
“Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack” Metadata:
- Title: ➤ Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack
- Author: M. Nallasamy
- Language: English
- Publisher: Lewis Research Center
- Publish Date: 1989
- Publish Location: Cleveland, Ohio
“Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack” Subjects and Themes:
- Subjects: Pressure distribution - Rotor aerodynamics - Unsteady aerodynamics - Propeller blades - Angle of attack
Edition Identifiers:
- The Open Library ID: OL16122158M
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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44Verfahren in der instationaren Aerodynamik
By Wolfgang Geissler
“Verfahren in der instationaren Aerodynamik” Metadata:
- Title: ➤ Verfahren in der instationaren Aerodynamik
- Author: Wolfgang Geissler
- Number of Pages: Median: 501
- Publisher: DLR
- Publish Date: 1993
- Publish Location: Koln
“Verfahren in der instationaren Aerodynamik” Subjects and Themes:
- Subjects: Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL19750735M
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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45Sensitivity analysis of flutter response of a wing incorporating finite-span corrections
By Jason C. Issac
“Sensitivity analysis of flutter response of a wing incorporating finite-span corrections” Metadata:
- Title: ➤ Sensitivity analysis of flutter response of a wing incorporating finite-span corrections
- Author: Jason C. Issac
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Sensitivity analysis of flutter response of a wing incorporating finite-span corrections” Subjects and Themes:
- Subjects: ➤ Aspect ratio - Sweep angle - Chebyshev approximation - Unsteady aerodynamics - Aerodynamic characteristics - Compressible flow - Aeroelasticity - Flutter - Wing span
Edition Identifiers:
- The Open Library ID: OL15506230M
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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Downloads Are Not Available:
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46Higher harmonic control analysis for vibration reduction of helicopter rotor systems
By Khanh Q. Nguyen
“Higher harmonic control analysis for vibration reduction of helicopter rotor systems” Metadata:
- Title: ➤ Higher harmonic control analysis for vibration reduction of helicopter rotor systems
- Author: Khanh Q. Nguyen
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
- Publish Date: 1994
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Higher harmonic control analysis for vibration reduction of helicopter rotor systems” Subjects and Themes:
- Subjects: ➤ Helicopters - Harmonic control - Rotary wings - Matrices (Mathematics) - Aerodynamic loads - Mathematical models - Newton methods - Structural design criteria - Finite element method - Rigid rotors - Vibration damping - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL15408643M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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47Computational test cases for a rectangular supercritical wing undergoing pitching oscillations
By Robert M. Bennett
“Computational test cases for a rectangular supercritical wing undergoing pitching oscillations” Metadata:
- Title: ➤ Computational test cases for a rectangular supercritical wing undergoing pitching oscillations
- Author: Robert M. Bennett
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“Computational test cases for a rectangular supercritical wing undergoing pitching oscillations” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Unsteady aerodynamics - Aircraft parts - Supercritical wings - Wind tunnel tests - Wing oscillations - Rectangular wings
Edition Identifiers:
- The Open Library ID: OL15548991M
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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Downloads Are Not Available:
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48Higher harmonic control analysis for vibration reduction of helicopter rotor systems
By Khánh Nguyẽ̂n
“Higher harmonic control analysis for vibration reduction of helicopter rotor systems” Metadata:
- Title: ➤ Higher harmonic control analysis for vibration reduction of helicopter rotor systems
- Author: Khánh Nguyẽ̂n
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Higher harmonic control analysis for vibration reduction of helicopter rotor systems” Subjects and Themes:
- Subjects: ➤ Helicopters - Harmonic control - Rotary wings - Matrices (Mathematics) - Aerodynamic loads - Mathematical models - Newton methods - Structural design criteria - Finite element method - Rigid rotors - Vibration damping - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL17114626M
Access and General Info:
- First Year Published: 1994
- 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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49Application of higher harmonic control to hingeless rotor systems
By Khánh Nguyẽ̂n
“Application of higher harmonic control to hingeless rotor systems” Metadata:
- Title: ➤ Application of higher harmonic control to hingeless rotor systems
- Author: Khánh Nguyẽ̂n
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Application of higher harmonic control to hingeless rotor systems” Subjects and Themes:
- Subjects: ➤ Flapping - Harmonic control - Rotary wings - Unsteady aerodynamics - Vibration - Aerodynamic loads - Actuators - Vibratory loads - Finite element method - Rigid rotors - Rotors - Optimal control - Torsion
Edition Identifiers:
- The Open Library ID: OL17115418M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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50Application 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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