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Subsonic Analysis Of 0.04 Scale F 16xl Models Using An Unstructured Euler Code by Wendy B. Lessard

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1Subsonic Analysis Of 0.04-Scale F-16XL Models Using An Unstructured Euler Code

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The subsonic flow field about an F-16XL airplane model configuration was investigated with an inviscid unstructured grid technique. The computed surface pressures were compared to wind-tunnel test results at Mach 0.148 for a range of angles of attack from 0 deg to 20 deg. To evaluate the effect of grid dependency on the solution, a grid study was performed in which fine, medium, and coarse grid meshes were generated. The off-surface vortical flow field was locally adapted and showed improved correlation to the wind-tunnel data when compared to the nonadapted flow field. Computational results are also compared to experimental five-hole pressure probe data. A detailed analysis of the off-body computed pressure contours, velocity vectors, and particle traces are presented and discussed.

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  • Title: ➤  Subsonic Analysis Of 0.04-Scale F-16XL Models Using An Unstructured Euler Code
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  • Language: English

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The book is available for download in "texts" format, the size of the file-s is: 20.18 Mbs, the file-s for this book were downloaded 263 times, the file-s went public at Mon May 23 2011.

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2NASA Technical Reports Server (NTRS) 19970001348: Subsonic Analysis Of 0.04-Scale F-16XL Models Using An Unstructured Euler Code

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The subsonic flow field about an F-16XL airplane model configuration was investigated with an inviscid unstructured grid technique. The computed surface pressures were compared to wind-tunnel test results at Mach 0.148 for a range of angles of attack from 0 deg to 20 deg. To evaluate the effect of grid dependency on the solution, a grid study was performed in which fine, medium, and coarse grid meshes were generated. The off-surface vortical flow field was locally adapted and showed improved correlation to the wind-tunnel data when compared to the nonadapted flow field. Computational results are also compared to experimental five-hole pressure probe data. A detailed analysis of the off-body computed pressure contours, velocity vectors, and particle traces are presented and discussed.

“NASA Technical Reports Server (NTRS) 19970001348: Subsonic Analysis Of 0.04-Scale F-16XL Models Using An Unstructured Euler Code” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19970001348: Subsonic Analysis Of 0.04-Scale F-16XL Models Using An Unstructured Euler Code
  • Author: ➤  
  • Language: English

“NASA Technical Reports Server (NTRS) 19970001348: Subsonic Analysis Of 0.04-Scale F-16XL Models Using An Unstructured Euler Code” Subjects and Themes:

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The book is available for download in "texts" format, the size of the file-s is: 50.18 Mbs, the file-s for this book were downloaded 63 times, the file-s went public at Thu Oct 13 2016.

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