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Computational Fluid Dynamics Prediction Of Subsonic Axisymmetric And Two Dimensional Heated Free Turbulent Air Jets. by Dewulf%2c Michael D.
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1Computational Fluid Dynamics Prediction Of Subsonic Axisymmetric And Two-dimensional Heated Free Turbulent Air Jets.
By DeWulf, Michael D.
A study was conducted to evaluate the accuracy of a commercial computational fluid dynamics (CFD) code (CFDRC-ACE+) for predicting incompressible air jet flows with simple geometries. Specifically, the axis- symmetric and two-dimensional heated air-jets were simulated using a standard k- epsilon turbulence model. These CFD predictions were directly compared to an extensive compilation of experimental data from archive literature. The round jet results indicated that the code over-predicted the velocity-spreading rate by 24% and the temperature spreading rate by 29%
“Computational Fluid Dynamics Prediction Of Subsonic Axisymmetric And Two-dimensional Heated Free Turbulent Air Jets.” Metadata:
- Title: ➤ Computational Fluid Dynamics Prediction Of Subsonic Axisymmetric And Two-dimensional Heated Free Turbulent Air Jets.
- Author: DeWulf, Michael D.
- Language: English
Edition Identifiers:
- Internet Archive ID: computationalflu1094532953
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 1316.65 Mbs, the file-s for this book were downloaded 87 times, the file-s went public at Fri Apr 26 2019.
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2DTIC ADA384691: Computational Fluid Dynamics Prediction Of Subsonic Axisymmetric And Two-Dimensional Heated Free Turbulent Air Jets
By Defense Technical Information Center
A study was conducted to evaluate the accuracy of a commercial computational fluid dynamics (CFD) code (CFDRC-ACE+) for predicting incompressible air jet flows with simple geometries. Specifically, the axis-symmetric and two-dimensional heated air-jets were simulated using a standard k-epsilon turbulence model. These CFD predictions were directly compared to an extensive compilation of experimental data from archive literature. The round jet results indicated that the code over-predicted the velocity-spreading rate by 24% and the temperature spreading rate by 29%.
“DTIC ADA384691: Computational Fluid Dynamics Prediction Of Subsonic Axisymmetric And Two-Dimensional Heated Free Turbulent Air Jets” Metadata:
- Title: ➤ DTIC ADA384691: Computational Fluid Dynamics Prediction Of Subsonic Axisymmetric And Two-Dimensional Heated Free Turbulent Air Jets
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA384691: Computational Fluid Dynamics Prediction Of Subsonic Axisymmetric And Two-Dimensional Heated Free Turbulent Air Jets” Subjects and Themes:
- Subjects: ➤ DTIC Archive - DeWulf, Michael D - NAVAL POSTGRADUATE SCHOOL MONTEREY CA - *COMPUTATIONAL FLUID DYNAMICS - VELOCITY - TEMPERATURE - AIR FLOW - TURBULENCE - MATHEMATICAL PREDICTION - JET FLOW - INCOMPRESSIBLE FLOW - AIRCRAFT EXHAUST
Edition Identifiers:
- Internet Archive ID: DTIC_ADA384691
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 104.14 Mbs, the file-s for this book were downloaded 50 times, the file-s went public at Mon Apr 30 2018.
Available formats:
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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