Explore: Aspect Ratio
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Source: The Open Library
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1Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
By Scott P. Fears
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Metadata:
- Title: ➤ Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
- Author: Scott P. Fears
- Language: English
- Number of Pages: Median: 145
- Publisher: ➤ National Aeronautics and Space Administration - Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Hampton, Va - [Washington, DC - Springfield, Va
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Subjects and Themes:
- Subjects: ➤ Trailing edge flaps - Aspect ratio - Flight stability tests - Stabilizers (Fluid dynamics) - Wind tunnel tests - Wing profiles - Aerodynamic stability - Angle of attack - Stability - Flight control - Low speed - Planforms - Arrow wings - Tail assemblies - Leading edge flaps
Edition Identifiers:
- The Open Library ID: OL19003591M - OL15416719M - OL18082907M - OL17032232M
- Online Computer Library Center (OCLC) ID: 34127880
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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2Experimental study of vortex breakdown in a cylindrical, swirling flow
“Experimental study of vortex breakdown in a cylindrical, swirling flow” Metadata:
- Title: ➤ Experimental study of vortex breakdown in a cylindrical, swirling flow
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Joint Institute for Aeronautics and Acoustics, Stanford University - Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Stanford, Calif.] - [Washington, DC
“Experimental study of vortex breakdown in a cylindrical, swirling flow” Subjects and Themes:
- Subjects: ➤ Axisymmetric flow - Vortex breakdown - Reynolds number - Steady flow - Flow stability - Cylindrical bodies - Swirling - Internal flow - Aspect ratio
Edition Identifiers:
- The Open Library ID: OL17838001M
- Online Computer Library Center (OCLC) ID: 40101976
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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3An aspect ratio bound for triangulating a d-grid cut by a hyperplane
By Scott A. Mitchell
“An aspect ratio bound for triangulating a d-grid cut by a hyperplane” Metadata:
- Title: ➤ An aspect ratio bound for triangulating a d-grid cut by a hyperplane
- Author: Scott A. Mitchell
- Language: English
- Publisher: ➤ Research Institute for Advanced Computer Science, NASA Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Moffett Field, Calif.]
“An aspect ratio bound for triangulating a d-grid cut by a hyperplane” Subjects and Themes:
- Subjects: Grid generation (Mathematics) - Hyperplanes - Aspect ratio - Computational grids - Finite element method
Edition Identifiers:
- The Open Library ID: OL15419134M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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4Buckling and postbuckling behavior of laminated composite plates with a cutout
By Michael P. Nemeth
“Buckling and postbuckling behavior of laminated composite plates with a cutout” Metadata:
- Title: ➤ Buckling and postbuckling behavior of laminated composite plates with a cutout
- Author: Michael P. Nemeth
- 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
“Buckling and postbuckling behavior of laminated composite plates with a cutout” Subjects and Themes:
- Subjects: Rectangular plates - Laminates - Composite materials - Aspect ratio - Buckling
Edition Identifiers:
- The Open Library ID: OL15504430M
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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5Sensitivity 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
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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6A comparison of structurally connected and multiple spacecraft interferometers
By Derek M. Surka
“A comparison of structurally connected and multiple spacecraft interferometers” Metadata:
- Title: ➤ A comparison of structurally connected and multiple spacecraft interferometers
- Author: Derek M. Surka
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“A comparison of structurally connected and multiple spacecraft interferometers” Subjects and Themes:
- Subjects: ➤ Interferometers - Structural stability - Attitude control - Actuators - Crossovers - Aspect ratio
Edition Identifiers:
- The Open Library ID: OL15547952M
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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7Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing
By M. D. Klinge
“Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing” Metadata:
- Title: ➤ Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing
- Author: M. D. Klinge
- Language: English
- Number of Pages: Median: 27
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1987
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Wings, Rectangular - Airplanes - Research - Rectangular wings - Flow visualization - Euler equations of motion - Flow distribution - Aspect ratio
- Places: United States
Edition Identifiers:
- The Open Library ID: OL17115139M
Access and General Info:
- First Year Published: 1987
- 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
Find Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.