Explore: High Aspect Ratio
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AI-Generated Overview About “high-aspect-ratio”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber
By Mary F. Wadel
“Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber” Metadata:
- Title: ➤ Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber
- Author: Mary F. Wadel
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber” Subjects and Themes:
- Subjects: ➤ High aspect ratio - Rocket engines - Performance tests - Mass flow - Cooling - Thrust chambers - Combustion chambers - Liquid hydrogen
Edition Identifiers:
- The Open Library ID: OL15496512M
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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2Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber
By Mary E. Wadel
“Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber” Metadata:
- Title: ➤ Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber
- Author: Mary E. Wadel
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber” Subjects and Themes:
- Subjects: ➤ Channels - Cooling - Design - Combustion chambers - Computer programs - High aspect ratio
Edition Identifiers:
- The Open Library ID: OL15503703M
Access and General Info:
- First Year Published: 1997
- 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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3The effect of cooling passage aspect ratio on curvature heat transfer enhancement
By Michael L. Meyer
“The effect of cooling passage aspect ratio on curvature heat transfer enhancement” Metadata:
- Title: ➤ The effect of cooling passage aspect ratio on curvature heat transfer enhancement
- Author: Michael L. Meyer
- Language: English
- Number of Pages: Median: 16
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1997
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“The effect of cooling passage aspect ratio on curvature heat transfer enhancement” Subjects and Themes:
- Subjects: ➤ Convective heat transfer - Heat transfer coefficients - High aspect ratio - Cooling - Curvature - Rocket engines - Heat - Secondary flow - Convection - Resistive heating - Rocket engine design
Edition Identifiers:
- The Open Library ID: OL16114768M
Access and General Info:
- First Year Published: 1997
- 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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4Electrically heated tube investigation of cooling channel geometry effects
By Michael L. Meyer
“Electrically heated tube investigation of cooling channel geometry effects” Metadata:
- Title: ➤ Electrically heated tube investigation of cooling channel geometry effects
- Author: Michael L. Meyer
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Electrically heated tube investigation of cooling channel geometry effects” Subjects and Themes:
- Subjects: ➤ Circular tubes - Heat transfer - Rocket engine design - Resistance heating - High aspect ratio - Cooling
Edition Identifiers:
- The Open Library ID: OL15414454M
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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5Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles
By James R. Burley
“Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles” Metadata:
- Title: ➤ Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles
- Author: James R. Burley
- 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: ➤ Springfield, Va - [Washington, D.C.]
“Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles” Subjects and Themes:
- Subjects: ➤ Testing - Nozzles - Air ducts - Wind tunnel tests - High aspect ratio - Static tests
Edition Identifiers:
- The Open Library ID: OL16114903M
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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6A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center
By Kenneth J. Davidian
“A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center” Metadata:
- Title: ➤ A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center
- Author: Kenneth J. Davidian
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.?]
“A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center” Subjects and Themes:
- Subjects: ➤ Nozzles - Rockets (Aeronautics) - Rocket nozzles - Nozzle geometry - High aspect ratio - Research facilities
Edition Identifiers:
- The Open Library ID: OL15419235M
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 A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center at online marketplaces:
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Aspect ratio (aeronautics)
Thus, a long, narrow wing has a high aspect ratio, whereas a short, wide wing has a low aspect ratio. Aspect ratio and other features of the planform
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
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
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
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
Bird wing
these types. These types of wings are elliptical wings, high-speed wings, high aspect ratio wings and soaring wings with slots. Elliptical wings are
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
21:9 aspect ratio
of this screen aspect ratio is a constant display height when displaying other content with a lesser aspect ratio. The 64:27 aspect ratio of "21:9" is an
Dry etching
wet etch to do anisotropic etching (removal of material) to create high aspect ratio structures (e.g. deep holes or capacitor trenches). The dry etching