Explore: Aspect Ratio
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Books Results
Source: The Open Library
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Search results from The Open Library
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.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Aspect ratio
The aspect ratio of a geometric shape is the ratio of its sizes in different dimensions. For example, the aspect ratio of a rectangle is the ratio of its
Aspect ratio (image)
The aspect ratio of an image is the ratio of its width to its height. It is expressed as two numbers separated by a colon, in the format width:height
Aspect ratio (aeronautics)
In aeronautics, the aspect ratio of a wing is the ratio of its span to its mean chord. It is equal to the square of the wingspan divided by the wing area
Display aspect ratio
The display aspect ratio (DAR) is the aspect ratio of a display device and so the proportional relationship between the physical width and the height of
Fullscreen (aspect ratio)
screen) refers to the 4:3 (1.33:1) aspect ratio of early standard television screens and computer monitors. Widescreen ratios started to become more popular
16:9 aspect ratio
aspect ratio with a width of 16 units and height of 9 units. Once seen as an "exotic" aspect ratio, since 2009, it has become the most common aspect ratio
List of national flags of sovereign states
"approximately 3:5" have been given as the flag's ratio. It has also been claimed the proportions are golden. 2:3 aspect ratio is a valid alternative Robert Heft has
Aspect ratio (disambiguation)
The aspect ratio of a geometric shape is the ratio of its sizes in different dimensions. Aspect ratio may also refer to: Aspect ratio (aeronautics), the
Pixel aspect ratio
A pixel aspect ratio (PAR) is a mathematical ratio that describes how the width of a pixel in a digital image compares to the height of that pixel. Most
16:10 aspect ratio
equivalent 8:5, is an aspect ratio commonly used for computer displays and tablet computers. It is equal to 8/5, close to the golden ratio ( φ {\displaystyle