Explore: Flutter
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Learn more about Flutter with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “flutter”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1In-flight investigation of a rotating cylinder-based structural excitation system for flutter testing
By Lura Vernon
“In-flight investigation of a rotating cylinder-based structural excitation system for flutter testing” Metadata:
- Title: ➤ In-flight investigation of a rotating cylinder-based structural excitation system for flutter testing
- Author: Lura Vernon
- Language: English
- Number of Pages: Median: 20
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - Dryden Flight Research Facility
- Publish Date: 1993
- Publish Location: ➤ Edwards, Calif - [Washington, DC] - [Springfield, Va
“In-flight investigation of a rotating cylinder-based structural excitation system for flutter testing” Subjects and Themes:
- Subjects: Aeroelasticity - Excitation - Flutter
Edition Identifiers:
- The Open Library ID: OL19750201M - OL15385164M - OL17110517M - OL16386519M - OL18064223M
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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2Flutter of a low-aspect-ratio rectangular wing
By Stanley R. Cole
“Flutter of a low-aspect-ratio rectangular wing” Metadata:
- Title: ➤ Flutter of a low-aspect-ratio rectangular wing
- Author: Stanley R. Cole
- Language: English
- Number of Pages: Median: 15
- Publisher: ➤ For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1989
- Publish Location: Hampton, Va - [Springfield, Va
“Flutter of a low-aspect-ratio rectangular wing” Subjects and Themes:
- Subjects: ➤ Airplanes - Flutter - Flutter (Aerodynamics) - Low aspect ratio wings - Rectangular wings - Wings, Rectangular
Edition Identifiers:
- The Open Library ID: OL15292377M - OL18033456M - OL17100416M - OL19379713M
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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3Evaluation of diffuse-illumination holographic cinematography in a flutter cascade
By Arthur J. Decker
“Evaluation of diffuse-illumination holographic cinematography in a flutter cascade” Metadata:
- Title: ➤ Evaluation of diffuse-illumination holographic cinematography in a flutter cascade
- Author: Arthur J. Decker
- Language: English
- Number of Pages: Median: 29
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Lewis Research Center - For sale by the National Technical Information Service]
- Publish Date: 1986 - 1987
- Publish Location: ➤ Cleveland, Ohio - [Springfield, Va - [Washington, D.C.]
“Evaluation of diffuse-illumination holographic cinematography in a flutter cascade” Subjects and Themes:
- Subjects: ➤ Holography - Holographic interferometry - Flow visualization - Neodymium lasers - Cascade wind tunnels - Flutter
Edition Identifiers:
- The Open Library ID: OL15275157M - OL20982795M - OL14663901M - OL18029094M
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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4Methods for in-flight robustness evaluation
By James D. Paduano
“Methods for in-flight robustness evaluation” Metadata:
- Title: ➤ Methods for in-flight robustness evaluation
- Author: James D. Paduano
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Methods for in-flight robustness evaluation” Subjects and Themes:
- Subjects: ➤ Applications programs (Computers) - Control theory - Flight control - Flutter - Flutter analysis - Prediction analysis techniques - Robustness (Mathematics)
Edition Identifiers:
- The Open Library ID: OL18119046M - OL15499053M - OL17572266M
- Online Computer Library Center (OCLC) ID: 39901038
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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5A worst-case approach for on-line flutter prediction
By Rick C. Lind
“A worst-case approach for on-line flutter prediction” Metadata:
- Title: ➤ A worst-case approach for on-line flutter prediction
- Author: Rick C. Lind
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“A worst-case approach for on-line flutter prediction” Subjects and Themes:
- Subjects: ➤ Flight tests - Dynamic structural analysis - Prediction analysis techniques - Flutter analysis - Aeroelasticity - Flutter - On-line systems
Edition Identifiers:
- The Open Library ID: OL18132111M - OL17700401M - OL17578595M
- Online Computer Library Center (OCLC) ID: 40763828
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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6Flow limitation and flutter in membrane walled collapsible tubes: a model for expiratory wheezing
By Colin Walsh
“Flow limitation and flutter in membrane walled collapsible tubes: a model for expiratory wheezing” Metadata:
- Title: ➤ Flow limitation and flutter in membrane walled collapsible tubes: a model for expiratory wheezing
- Author: Colin Walsh
- Language: English
- Number of Pages: Median: 254
- Publisher: University of Toronto
- Publish Date: 1992
- Publish Location: [Downsview, Ont.]
“Flow limitation and flutter in membrane walled collapsible tubes: a model for expiratory wheezing” Subjects and Themes:
- Subjects: Air flow - Collapsible tubes - Flutter - Wheezing
Edition Identifiers:
- The Open Library ID: OL21811112M - OL19243418M
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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7Overview of recent flight flutter testing research at NASA Dryden
By Martin J. Brenner
“Overview of recent flight flutter testing research at NASA Dryden” Metadata:
- Title: ➤ Overview of recent flight flutter testing research at NASA Dryden
- Author: Martin J. Brenner
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1997
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Overview of recent flight flutter testing research at NASA Dryden” Subjects and Themes:
- Subjects: ➤ Aeroservoelasticity - Flight tests - Flutter - Research aircraft - Signal processing - System identification - Wavelet analysis
Edition Identifiers:
- The Open Library ID: OL17593990M - OL15504658M
- Online Computer Library Center (OCLC) ID: 40458326
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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8Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model
By Charles L. Ruhlin
“Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model” Metadata:
- Title: ➤ Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model
- Author: Charles L. Ruhlin
- Language: English
- Number of Pages: Median: 73
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1986 - 1987
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, D.C.]
“Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Transonic flutter - Flutter (Aerodynamics) - Winglets - Flutter - Structural engineering
- Places: United States
Edition Identifiers:
- The Open Library ID: OL14663625M - OL20986071M
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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9Ground vibration test of an F-16 airplane with modified decoupler pylons
By F. W. Cazier
“Ground vibration test of an F-16 airplane with modified decoupler pylons” Metadata:
- Title: ➤ Ground vibration test of an F-16 airplane with modified decoupler pylons
- Author: F. W. Cazier
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ Springfield, Va - Washington, D.C
“Ground vibration test of an F-16 airplane with modified decoupler pylons” Subjects and Themes:
- Subjects: ➤ Testing - F-16 (Jet fighter plane) - Vibration (Aeronautics) - Vibration isolators - F-16 aircraft - Vibration tests - External tanks - Ground tests - Vibration mode - Flutter - Pylons
Edition Identifiers:
- The Open Library ID: OL17634634M - OL17727207M
- Online Computer Library Center (OCLC) ID: 166343313
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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10Correlation filtering of modal dynamics using the Laplace wavelet
By Lawrence C. Freudinger
“Correlation filtering of modal dynamics using the Laplace wavelet” Metadata:
- Title: ➤ Correlation filtering of modal dynamics using the Laplace wavelet
- Author: Lawrence C. Freudinger
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Correlation filtering of modal dynamics using the Laplace wavelet” Subjects and Themes:
- Subjects: Wavelet analysis - Systems health monitoring - Algorithms - Flutter - Correlation
Edition Identifiers:
- The Open Library ID: OL15547505M - OL17583513M
- Online Computer Library Center (OCLC) ID: 41663719
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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11Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods
By Lawrence C. Freudinger
“Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods” Metadata:
- Title: ➤ Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods
- Author: Lawrence C. Freudinger
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: ➤ [Washington, D.C.] - [Springfield, VA
“Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods” Subjects and Themes:
- Subjects: ➤ Vibration - Flutter (Aerodynamics) - Hornet (Jet fighter plane) - Research aircraft - F-18 aircraft - Wing tips - Angle of attack - Clearances - Flutter
Edition Identifiers:
- The Open Library ID: OL17630290M - OL16139104M
- Online Computer Library Center (OCLC) ID: 24899921
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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12Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
By Osama A. Kandil
“Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications” Metadata:
- Title: ➤ Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
- Author: Osama A. Kandil
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Norfolk, Va - Springfield, Va
“Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Buffeting - Computational fluid dynamics - Delta wings - Flutter - Vortices - Wing tips
Edition Identifiers:
- The Open Library ID: OL17593616M - OL15508543M
- Online Computer Library Center (OCLC) ID: 40618623
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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13FPCAS3D 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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14Improved flight test procedures for flutter clearance
By Rick C. Lind
“Improved flight test procedures for flutter clearance” Metadata:
- Title: ➤ Improved flight test procedures for flutter clearance
- Author: Rick C. Lind
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Improved flight test procedures for flutter clearance” Subjects and Themes:
- Subjects: ➤ Dynamic response - Flight envelopes - Clearances - Flight tests - Environmental monitoring - Research aircraft - Aeroelasticity - Flutter
Edition Identifiers:
- The Open Library ID: OL17583514M - OL15547508M
- Online Computer Library Center (OCLC) ID: 41667675
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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15Design, test, and evaluation of three active flutter suppression controllers
By William M. Adams
“Design, test, and evaluation of three active flutter suppression controllers” Metadata:
- Title: ➤ Design, test, and evaluation of three active flutter suppression controllers
- Author: William M. Adams
- Number of Pages: Median: 38
- Publisher: Langley Research Center
- Publish Date: 1992
- Publish Location: Hampton, Va
“Design, test, and evaluation of three active flutter suppression controllers” Subjects and Themes:
- Subjects: Controllers - Flutter
Edition Identifiers:
- The Open Library ID: OL19246427M
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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16Numerical integration methods for supersonic wings in steady and oscillatory motion
By Bernard Etkin
“Numerical integration methods for supersonic wings in steady and oscillatory motion” Metadata:
- Title: ➤ Numerical integration methods for supersonic wings in steady and oscillatory motion
- Author: Bernard Etkin
- Number of Pages: Median: 37
- Publisher: Institute of Aerophysics
- Publish Date: 1955
- Publish Location: [Downsview, Ont.]
“Numerical integration methods for supersonic wings in steady and oscillatory motion” Subjects and Themes:
- Subjects: Supersonic flow - Flutter - Wings
Edition Identifiers:
- The Open Library ID: OL20897574M
Access and General Info:
- First Year Published: 1955
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17Preliminary investigation of the air loads on an oscillating two-dimensional aerofoil with leading and trailing edge flap, with emphasis on the negative stall
By D. R. Madill
“Preliminary investigation of the air loads on an oscillating two-dimensional aerofoil with leading and trailing edge flap, with emphasis on the negative stall” Metadata:
- Title: ➤ Preliminary investigation of the air loads on an oscillating two-dimensional aerofoil with leading and trailing edge flap, with emphasis on the negative stall
- Author: D. R. Madill
- Number of Pages: Median: 44
- Publisher: ➤ Dept. of Aeronautical Engineering
- Publish Date: 1959
- Publish Location: [Downsview, Ont.]
“Preliminary investigation of the air loads on an oscillating two-dimensional aerofoil with leading and trailing edge flap, with emphasis on the negative stall” Subjects and Themes:
- Subjects: Aerodynamic derivatives - Flutter
Edition Identifiers:
- The Open Library ID: OL22344632M
Access and General Info:
- First Year Published: 1959
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Final technical report for aeroelastic analysis of counter rotation fans
By Theo G. Keith
“Final technical report for aeroelastic analysis of counter rotation fans” Metadata:
- Title: ➤ Final technical report for aeroelastic analysis of counter rotation fans
- Author: Theo G. Keith
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Final technical report for aeroelastic analysis of counter rotation fans” Subjects and Themes:
- Subjects: ➤ Prop-fan technology - Aerodynamic loads - Turbomachinery - Counter rotation - Dynamic characteristics - Aeroelasticity - Flutter - Fatigue life
Edition Identifiers:
- The Open Library ID: OL18131915M
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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19Final technical report for aeroelastic analysis of turbomachinery for space propulsion
By Theo G. Keith
“Final technical report for aeroelastic analysis of turbomachinery for space propulsion” Metadata:
- Title: ➤ Final technical report for aeroelastic analysis of turbomachinery for space propulsion
- Author: Theo G. Keith
- Language: English
- Publisher: ➤ Dept. of Mechanical, Industrial and Manufacturing Engineering, University of Toledo - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - Toledo, Ohio - [Washington, DC
“Final technical report for aeroelastic analysis of turbomachinery for space propulsion” Subjects and Themes:
- Subjects: Thrust - Propulsion - Aeroelasticity - Flutter - Turbomachinery
Edition Identifiers:
- The Open Library ID: OL18136743M
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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20Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations
By Theo G. Keith
“Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations” Metadata:
- Title: ➤ Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations
- Author: Theo G. Keith
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations” Subjects and Themes:
- Subjects: Ducted fans - Fan blades - Navier-Stokes equation - Flutter - Flow distribution
Edition Identifiers:
- The Open Library ID: OL18134780M
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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21Unstalled flutter stability predictions and comparisions [sic] to test data for a composite prop-fan model
By Jay E. Turnberg
“Unstalled flutter stability predictions and comparisions [sic] to test data for a composite prop-fan model” Metadata:
- Title: ➤ Unstalled flutter stability predictions and comparisions [sic] to test data for a composite prop-fan model
- Author: Jay E. Turnberg
- Language: English
- Publisher: ➤ Hamilton Standard Division, United Technologies Corp. - National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1986
- Publish Location: ➤ [Windsor Locks, CT] - [Washington, D.C - Springfield, Va
“Unstalled flutter stability predictions and comparisions [sic] to test data for a composite prop-fan model” Subjects and Themes:
- Subjects: ➤ Prop-fan technology - Structural analysis - Prediction analysis techniques - Aeroelasticity - Rotor blades (Turbomachinery) - Flutter
Edition Identifiers:
- The Open Library ID: OL15411898M
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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22The use of the Regier number in the structural design with flutter constraints
By H. J. Dunn
“The use of the Regier number in the structural design with flutter constraints” Metadata:
- Title: ➤ The use of the Regier number in the structural design with flutter constraints
- Author: H. J. Dunn
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, Va
“The use of the Regier number in the structural design with flutter constraints” Subjects and Themes:
- Subjects: ➤ Optimization - Aeroelasticity - Aircraft design - Structural design - Wings - Flutter
Edition Identifiers:
- The Open Library ID: OL15403923M
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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23Analytical and experimental investigation of flutter suppression by piezoelectric actuation
By Jennifer Heeg
“Analytical and experimental investigation of flutter suppression by piezoelectric actuation” Metadata:
- Title: ➤ Analytical and experimental investigation of flutter suppression by piezoelectric actuation
- Author: Jennifer Heeg
- Number of Pages: Median: 43
- Publisher: Langley Research Center
- Publish Date: 1993
- Publish Location: Hampton, Va
“Analytical and experimental investigation of flutter suppression by piezoelectric actuation” Subjects and Themes:
- Subjects: Actuators - Piezoelectricity - Flutter
Edition Identifiers:
- The Open Library ID: OL22346172M
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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24Aeroelastic flutter and divergence of rectangular wings with bending-torsion coupling
By Harry Penick Selby
“Aeroelastic flutter and divergence of rectangular wings with bending-torsion coupling” Metadata:
- Title: ➤ Aeroelastic flutter and divergence of rectangular wings with bending-torsion coupling
- Author: Harry Penick Selby
- Number of Pages: Median: 182
- Publisher: ➤ Massachusetts Institute of Technology
- Publish Date: 1982
- Publish Location: [Cambridge, Mass.]
“Aeroelastic flutter and divergence of rectangular wings with bending-torsion coupling” Subjects and Themes:
- Subjects: Aeroelastic research wings - Divergence - Flutter
Edition Identifiers:
- The Open Library ID: OL18929354M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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25Aeroelastic flutter and divergence of graphite/epoxy cantilevered plates with bending-torsion stiffness coupling
By Steven James Hollowell
“Aeroelastic flutter and divergence of graphite/epoxy cantilevered plates with bending-torsion stiffness coupling” Metadata:
- Title: ➤ Aeroelastic flutter and divergence of graphite/epoxy cantilevered plates with bending-torsion stiffness coupling
- Author: Steven James Hollowell
- Publisher: ➤ Massachusetts Institute of Technology
- Publish Date: 1981
- Publish Location: [Cambridge, Mass.]
“Aeroelastic flutter and divergence of graphite/epoxy cantilevered plates with bending-torsion stiffness coupling” Subjects and Themes:
- Subjects: Aeroelastic research wings - Flutter - Graphite-epoxy composites
Edition Identifiers:
- The Open Library ID: OL18929362M
Access and General Info:
- First Year Published: 1981
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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26Approximate calculation of the pressure distribution on a rectangular wing oscillating in incompressible flow
By E. D. Poppleton
“Approximate calculation of the pressure distribution on a rectangular wing oscillating in incompressible flow” Metadata:
- Title: ➤ Approximate calculation of the pressure distribution on a rectangular wing oscillating in incompressible flow
- Author: E. D. Poppleton
- Number of Pages: Median: 26
- Publisher: Institute of Aerophysics
- Publish Date: 1958
- Publish Location: [Downsview, Ont.]
“Approximate calculation of the pressure distribution on a rectangular wing oscillating in incompressible flow” Subjects and Themes:
- Subjects: Pressure distribution - Unsteady flow - Flutter - Wings
Edition Identifiers:
- The Open Library ID: OL19251806M
Access and General Info:
- First Year Published: 1958
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27ASTROP2 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
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28User'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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29Design and fabrication of the NASA decoupler pylon for the F-16 aircraft
By J. D. Clayton
“Design and fabrication of the NASA decoupler pylon for the F-16 aircraft” Metadata:
- Title: ➤ Design and fabrication of the NASA decoupler pylon for the F-16 aircraft
- Author: J. D. Clayton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - General Dynamics, Fort Worth Division
- Publish Date: 1985
- Publish Location: Hampton, Va - Fort Worth, Tex
“Design and fabrication of the NASA decoupler pylon for the F-16 aircraft” Subjects and Themes:
- Subjects: ➤ Pylons - Flutter (Aerodynamics) - Wind tunnel tests - Structural design criteria - Flutter - Wing-fuselage stores - F-16 (Jet fighter plane) - Aeroelasticity - Flight tests
Edition Identifiers:
- The Open Library ID: OL18295927M
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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30Aeroelastic calculations using CFD for a typical business jet model
By Michael D. Gibbons
“Aeroelastic calculations using CFD for a typical business jet model” Metadata:
- Title: ➤ Aeroelastic calculations using CFD for a typical business jet model
- Author: Michael D. Gibbons
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor
- Publish Date: 1996
- Publish Location: Springfield, VA - Hampton, Va
“Aeroelastic calculations using CFD for a typical business jet model” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Viscous flow - Flexible wings - Navier-Stokes equation - Aerodynamic coefficients - Aeroelasticity - Flutter
Edition Identifiers:
- The Open Library ID: OL15490455M
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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31A note on the T-tail flutter
By Kyuichiro Washizu
“A note on the T-tail flutter” Metadata:
- Title: A note on the T-tail flutter
- Author: Kyuichiro Washizu
- Number of Pages: Median: 15
- Publisher: Royal Aircraft Establishment
- Publish Date: 1971
- Publish Location: [S.l.]
“A note on the T-tail flutter” Subjects and Themes:
- Subjects: Lateral stability - T tail - Flutter
Edition Identifiers:
- The Open Library ID: OL20982399M
Access and General Info:
- First Year Published: 1971
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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32Effect of control surface mass unbalance on the stability of a closed-loop active control system
By E. Nissim
“Effect of control surface mass unbalance on the stability of a closed-loop active control system” Metadata:
- Title: ➤ Effect of control surface mass unbalance on the stability of a closed-loop active control system
- Author: E. Nissim
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - National Technical Information Service, distributor]
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Effect of control surface mass unbalance on the stability of a closed-loop active control system” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Feedback control - Aerodynamic stability - Flutter - Mass distribution - Control surfaces - Balance - Inertia - Active control
Edition Identifiers:
- The Open Library ID: OL15402406M
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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33Method for experimental determination of flutter speed by parameter identification
By E. Nissim
“Method for experimental determination of flutter speed by parameter identification” Metadata:
- Title: ➤ Method for experimental determination of flutter speed by parameter identification
- Author: E. Nissim
- Language: English
- Number of Pages: Median: 40
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service
- Publish Date: 1989
- Publish Location: ➤ [Washington, D.C.] - Springfield, VA
“Method for experimental determination of flutter speed by parameter identification” Subjects and Themes:
- Subjects: ➤ Flutter (Aerodynamics) - Parameter identification - Dynamic pressure - Mathematical models - Aeroelasticity - Flutter - Flight tests
Edition Identifiers:
- The Open Library ID: OL16123560M
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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34Research and applications in structures at the NASA Langley Research Center
By Irving Abel
“Research and applications in structures at the NASA Langley Research Center” Metadata:
- Title: ➤ Research and applications in structures at the NASA Langley Research Center
- Author: Irving Abel
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: Hampton, Va - [Springfield, Va
“Research and applications in structures at the NASA Langley Research Center” Subjects and Themes:
- Subjects: ➤ Test facilities - Composite materials - Dynamic structural analysis - Aeroelasticity - Smart structures - Flutter - Research
Edition Identifiers:
- The Open Library ID: OL17516405M
- Online Computer Library Center (OCLC) ID: 38068772
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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35Aeroelasticity of wing and wing-body configurations on parallel computers
By Chansup Byun
“Aeroelasticity of wing and wing-body configurations on parallel computers” Metadata:
- Title: ➤ Aeroelasticity of wing and wing-body configurations on parallel computers
- Author: Chansup Byun
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - MCAT Institute - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - San Jose, CA - [Washington, DC
“Aeroelasticity of wing and wing-body configurations on parallel computers” Subjects and Themes:
- Subjects: ➤ Parallel computers - Body-wing configurations - Aircraft configurations - Parallel processing (Computers) - Computer aided design - Aerodynamic configurations - Aeroelasticity - Aircraft design - Flutter
Edition Identifiers:
- The Open Library ID: OL15413748M
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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36Optical measurement of unducted fan flutter
By Anatole P Kurkov
“Optical measurement of unducted fan flutter” Metadata:
- Title: ➤ Optical measurement of unducted fan flutter
- Author: Anatole P Kurkov
- Language: English
- Publisher: ➤ NASA - National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Optical measurement of unducted fan flutter” Subjects and Themes:
- Subjects: ➤ Optical measurement - Nonlinearity - Blade tips - Counter rotation - Rotors - Vibration mode - Aeroelasticity - Flutter - Centrifugal force
Edition Identifiers:
- The Open Library ID: OL15404767M
Author's Alternative Names:
"Anatole P. Kurkov"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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37Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model
By Walter A. Silva
“Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model” Metadata:
- Title: ➤ Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model
- Author: Walter A. Silva
- Language: English
- Number of Pages: Median: 11
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Flutter analysis - Mathematical models - Flexible wings - Performance prediction - Perturbation theory - Wind tunnel models - Flutter
Edition Identifiers:
- The Open Library ID: OL16138056M
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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38The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis
By Qiangang Liu
“The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis” Metadata:
- Title: ➤ The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis
- Author: Qiangang Liu
- Number of Pages: Median: 23
- Publisher: ➤ Institute for Aerospace Studies
- Publish Date: 1986
- Publish Location: [Downsview, Ont.]
“The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis” Subjects and Themes:
- Subjects: Panel method (Fluid dynamics) - Flutter - Green's functions
Edition Identifiers:
- The Open Library ID: OL19985873M
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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39Sensitivity 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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40Flutter clearance of the F-14A variable-sweep transition flight experiment airplane
By Lawrence C. Freudinger
“Flutter clearance of the F-14A variable-sweep transition flight experiment airplane” Metadata:
- Title: ➤ Flutter clearance of the F-14A variable-sweep transition flight experiment airplane
- Author: Lawrence C. Freudinger
- Language: English
- Number of Pages: Median: 39
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
- Publish Date: 1990
- Publish Location: ➤ [Springfield, VA - Edwards, Calif
“Flutter clearance of the F-14A variable-sweep transition flight experiment airplane” Subjects and Themes:
- Subjects: ➤ Variable sweep wings - Flutter (Aerodynamics) - F-14 aircraft - Flight tests - Laminar flow - Flutter
Edition Identifiers:
- The Open Library ID: OL16131098M
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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41Bibliography of vibration and flutter of aircraft wings and control surfaces
By Alexander Klemin
“Bibliography of vibration and flutter of aircraft wings and control surfaces” Metadata:
- Title: ➤ Bibliography of vibration and flutter of aircraft wings and control surfaces
- Author: Alexander Klemin
- Number of Pages: Median: 337
- Publisher: ➤ U. S. Works Progress Administration
- Publish Date: 1937
- Publish Location: [New York?]
“Bibliography of vibration and flutter of aircraft wings and control surfaces” Subjects and Themes:
- Subjects: Control surfaces - Vibration - Bibliography - Wings - Flutter
Edition Identifiers:
- The Open Library ID: OL19248861M
Access and General Info:
- First Year Published: 1937
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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42AGARD standard aeroelastic configurations for dynamic response: I - Wing 445.6
By E. Carson Yates
“AGARD standard aeroelastic configurations for dynamic response: I - Wing 445.6” Metadata:
- Title: ➤ AGARD standard aeroelastic configurations for dynamic response: I - Wing 445.6
- Author: E. Carson Yates
- Number of Pages: Median: 33
- Publisher: AGARD
- Publish Date: 1988
- Publish Location: Neuilly sur Seine, France
“AGARD standard aeroelastic configurations for dynamic response: I - Wing 445.6” Subjects and Themes:
- Subjects: Aeroelasticity - Swept wings - Flutter
Edition Identifiers:
- The Open Library ID: OL18927273M
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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43A worst-case approach for on-line flutter prediction
By Rick Lind
“A worst-case approach for on-line flutter prediction” Metadata:
- Title: ➤ A worst-case approach for on-line flutter prediction
- Author: Rick Lind
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“A worst-case approach for on-line flutter prediction” Subjects and Themes:
- Subjects: ➤ Flight tests - Dynamic structural analysis - Prediction analysis techniques - Flutter analysis - Aeroelasticity - Flutter - On-line systems
Edition Identifiers:
- The Open Library ID: OL17128556M
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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44Theory of aerodynamic instability and the mechanism of flutter
By Theodore Theodorsen
“Theory of aerodynamic instability and the mechanism of flutter” Metadata:
- Title: ➤ Theory of aerodynamic instability and the mechanism of flutter
- Author: Theodore Theodorsen
- Number of Pages: Median: 23
- Publisher: NACA
- Publish Date: 1935
- Publish Location: Washington
“Theory of aerodynamic instability and the mechanism of flutter” Subjects and Themes:
- Subjects: Flutter - Aerodynamic stability
Edition Identifiers:
- The Open Library ID: OL19379581M
Access and General Info:
- First Year Published: 1935
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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45Planform curvature effects on flutter characteristics of a wing with 56 degree leading-edge sweep and panel aspect ratio of 1.14
By Donald F. Keller
“Planform curvature effects on flutter characteristics of a wing with 56 degree leading-edge sweep and panel aspect ratio of 1.14” Metadata:
- Title: ➤ Planform curvature effects on flutter characteristics of a wing with 56 degree leading-edge sweep and panel aspect ratio of 1.14
- Author: Donald F. Keller
- Number of Pages: Median: 43
- Publisher: Langley Research Center
- Publish Date: 1991
- Publish Location: Hampton, Va
“Planform curvature effects on flutter characteristics of a wing with 56 degree leading-edge sweep and panel aspect ratio of 1.14” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL21499606M
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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46Span reduction effects on flutter characteristics of arrow-wing supersonic transport configurations
By Donald F. Keller
“Span reduction effects on flutter characteristics of arrow-wing supersonic transport configurations” Metadata:
- Title: ➤ Span reduction effects on flutter characteristics of arrow-wing supersonic transport configurations
- Author: Donald F. Keller
- Language: English
- Number of Pages: Median: 52
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service
- Publish Date: 1991
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Span reduction effects on flutter characteristics of arrow-wing supersonic transport configurations” Subjects and Themes:
- Subjects: ➤ Span reduction effects - Transonic - Flutter (Aerodynamics) - Arrow wing - Testing - Airplanes - Wings - Supersonic transport planes - Aeroelasticity - Supersonic transport - Flutter - High-speed civil transport
Edition Identifiers:
- The Open Library ID: OL16109849M
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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47Application 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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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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48Aeroelasticity and unsteady aerodynamics
By F. O. Carta
“Aeroelasticity and unsteady aerodynamics” Metadata:
- Title: ➤ Aeroelasticity and unsteady aerodynamics
- Author: F. O. Carta
- Number of Pages: Median: 54
- Publisher: ➤ United Technologies Research Center
- Publish Date: 1978
- Publish Location: [S.l.]
“Aeroelasticity and unsteady aerodynamics” Subjects and Themes:
- Subjects: Aeroelasticity - Unsteady flow - Flutter
Edition Identifiers:
- The Open Library ID: OL18928274M
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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49A presentation on robust flutter margin analysis and a flutterometer
By Rick C. Lind
“A presentation on robust flutter margin analysis and a flutterometer” Metadata:
- Title: ➤ A presentation on robust flutter margin analysis and a flutterometer
- Author: Rick C. Lind
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“A presentation on robust flutter margin analysis and a flutterometer” Subjects and Themes:
- Subjects: ➤ Flight envelopes - Commercial aircraft - Flutter analysis - Dynamic tests - Flight tests - Error analysis - Flutter
Edition Identifiers:
- The Open Library ID: OL15498527M
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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50Response of the alliance 1 proof-of-concept airplane under gust loads
By A. S. Naser
“Response of the alliance 1 proof-of-concept airplane under gust loads” Metadata:
- Title: ➤ Response of the alliance 1 proof-of-concept airplane under gust loads
- Author: A. S. Naser
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2001
- Publish Location: Hanover, MD - Hampton, Va
“Response of the alliance 1 proof-of-concept airplane under gust loads” Subjects and Themes:
- Subjects: ➤ Flexible wings - Wing loading - Flow stability - Gust loads - Gusts - Von Karman equation - Aeroelasticity - Flutter
Edition Identifiers:
- The Open Library ID: OL16030606M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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