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Strategies For Effectively Visualizing A 3d Flow Using Volume Line Integral Convolution
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1DTIC ADA329113: Strategies For Effectively Visualizing A 3D Flow Using Volume Line Integral Convolution.
By Defense Technical Information Center
This paper discusses strategies for effectively portraying 3D flow using volume line integral convolution. Issues include defining an appropriate input texture, clarifying the distinct identities and relative depths of the advected texture elements, and selectively highlighting regions of interest in both the input and output volumes. A part from offering insights into the greater potential of 3D LIC as a method for effectively representing flow in a volume, a principal contribution of this work is the suggestion of a technique for generating and rendering 3D visibility-impeding 'halos' that can help to intuitively indicate the presence of depth discontinuities between contiguous elements in a projection and thereby clarify the 3D spatial organization of elements in the flow. The proposed techniques are applied to the visualization of a hot, supersonic, laminar jet exiting into a colder, subsonic coflow.
“DTIC ADA329113: Strategies For Effectively Visualizing A 3D Flow Using Volume Line Integral Convolution.” Metadata:
- Title: ➤ DTIC ADA329113: Strategies For Effectively Visualizing A 3D Flow Using Volume Line Integral Convolution.
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA329113: Strategies For Effectively Visualizing A 3D Flow Using Volume Line Integral Convolution.” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Interrante, Victoria - INSTITUTE FOR COMPUTER APPLICATIONS IN SCIENCE AND ENGINEERING HAMPTON VA - *THREE DIMENSIONAL FLOW - *CONVOLUTION INTEGRALS - INPUT - OUTPUT - VOLUME - INTEGRALS - FLOW VISUALIZATION - DEPTH - DISCONTINUITIES - LAMINAR FLOW - JET FLOW.
Edition Identifiers:
- Internet Archive ID: DTIC_ADA329113
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 20.37 Mbs, the file-s for this book were downloaded 47 times, the file-s went public at Sat Apr 07 2018.
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Abbyy GZ - Additional Text PDF - Archive BitTorrent - DjVuTXT - Djvu XML - Image Container PDF - JPEG Thumb - Metadata - OCR Page Index - OCR Search Text - Page Numbers JSON - Scandata - Single Page Processed JP2 ZIP - chOCR - hOCR -
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2NASA Technical Reports Server (NTRS) 19970028779: Strategies For Effectively Visualizing A 3D Flow Using Volume Line Integral Convolution
By NASA Technical Reports Server (NTRS)
This paper discusses strategies for effectively portraying 3D flow using volume line integral convolution. Issues include defining an appropriate input texture, clarifying the distinct identities and relative depths of the advected texture elements, and selectively highlighting regions of interest in both the input and output volumes. Apart from offering insights into the greater potential of 3D LIC as a method for effectively representing flow in a volume, a principal contribution of this work is the suggestion of a technique for generating and rendering 3D visibility-impeding 'halos' that can help to intuitively indicate the presence of depth discontinuities between contiguous elements in a projection and thereby clarify the 3D spatial organization of elements in the flow. The proposed techniques are applied to the visualization of a hot, supersonic, laminar jet exiting into a colder, subsonic coflow.
“NASA Technical Reports Server (NTRS) 19970028779: Strategies For Effectively Visualizing A 3D Flow Using Volume Line Integral Convolution” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19970028779: Strategies For Effectively Visualizing A 3D Flow Using Volume Line Integral Convolution
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19970028779: Strategies For Effectively Visualizing A 3D Flow Using Volume Line Integral Convolution” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - SUPERSONIC JET FLOW - LAMINAR FLOW - HALOS - THREE DIMENSIONAL BOUNDARY LAYER - THREE DIMENSIONAL MODELS - FLOW VISUALIZATION - VISIBILITY - TEXTURES - JET FLOW - IDENTITIES - Interrante, Victoria - Grosch, Chester
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19970028779
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 12.99 Mbs, the file-s for this book were downloaded 52 times, the file-s went public at Fri Oct 14 2016.
Available formats:
Abbyy GZ - Animated GIF - Archive BitTorrent - DjVuTXT - Djvu XML - Item Tile - Metadata - Scandata - Single Page Processed JP2 ZIP - Text PDF -
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- Internet Archive: Details
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