Explore: Transonic Flutter
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Books Results
Source: The Open Library
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1Nonlinear aspects of transonic aeroelasticity
By Hema Sandhyarani Murty
“Nonlinear aspects of transonic aeroelasticity” Metadata:
- Title: ➤ Nonlinear aspects of transonic aeroelasticity
- Author: Hema Sandhyarani Murty
- Language: English
- Number of Pages: Median: 126
- Publisher: ➤ University of Toronto, Institute for Aerospace Studies - Institute for Aerospace Studies, University of Toronto
- Publish Date: 1992 - 1993
- Publish Location: ➤ [Downsview, Ont.] - [Toronto, Ont.]
“Nonlinear aspects of transonic aeroelasticity” Subjects and Themes:
- Subjects: ➤ Transonic flutter - Nonlinearity - Flutter analysis - Transonic flow - Areoelasticity - Aeroelasticity
Edition Identifiers:
- The Open Library ID: OL19248491M - OL19243878M - OL21810996M
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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2Transonic 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
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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3Effects 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
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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4Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
By Euromech Colloquium (349th 1996 Göttingen, Germany)
“Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Metadata:
- Title: ➤ Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
- Author: ➤ Euromech Colloquium (349th 1996 Göttingen, Germany)
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Subjects and Themes:
- Subjects: ➤ Airfoil oscillations - Airfoils - Boundary layer separation - Computational fluid dynamics - Coupling - Mach number - Separated flow - Transonic flow - Transonic flutter - Transonic speed - Unsteady flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL17595884M - OL15518388M
- Online Computer Library Center (OCLC) ID: 42671384
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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.
Online Borrowing:
Online Marketplaces
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5Future research on transonic unsteady aerodynamics and its aeroelastic applications
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Future research on transonic unsteady aerodynamics and its aeroelastic applications” Metadata:
- Title: ➤ Future research on transonic unsteady aerodynamics and its aeroelastic applications
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Publisher: AGARD
- Publish Date: 1987
- Publish Location: Neuilly sur Seine, France
“Future research on transonic unsteady aerodynamics and its aeroelastic applications” Subjects and Themes:
- Subjects: Aerodynamics - Aeroelasticity - Transonic flutter - Unsteady state
Edition Identifiers:
- The Open Library ID: OL19250093M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
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6Numerical study of transonic flutter of a two dimensional airfoil
By Koji Isogai
“Numerical study of transonic flutter of a two dimensional airfoil” Metadata:
- Title: ➤ Numerical study of transonic flutter of a two dimensional airfoil
- Author: Koji Isogai
- Number of Pages: Median: 25
- Publisher: National Aerospace Laboratory
- Publish Date: 1980
- Publish Location: Tokyo
“Numerical study of transonic flutter of a two dimensional airfoil” Subjects and Themes:
- Subjects: Transonic flutter
Edition Identifiers:
- The Open Library ID: OL21333145M
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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