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Automatic Computation Of Euler Marching And Subsonic Grids For Wing Fuselage Configurations by Raymond L. Barger
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1NASA Technical Reports Server (NTRS) 19940032443: Automatic Computation Of Euler-marching And Subsonic Grids For Wing-fuselage Configurations
By NASA Technical Reports Server (NTRS)
Algebraic procedures are described for the automatic generation of structured, single-block flow computation grids for relatively simple configurations (wing, fuselage, and fin). For supersonic flows, a quasi two-dimensional grid for Euler-marching codes is developed, and some sample results in graphical form are included. A type of grid for subsonic flow calculation is also described. The techniques are algebraic and are based on a generalization of the method of transfinite interpolation.
“NASA Technical Reports Server (NTRS) 19940032443: Automatic Computation Of Euler-marching And Subsonic Grids For Wing-fuselage Configurations” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19940032443: Automatic Computation Of Euler-marching And Subsonic Grids For Wing-fuselage Configurations
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19940032443: Automatic Computation Of Euler-marching And Subsonic Grids For Wing-fuselage Configurations” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - BODY-WING CONFIGURATIONS - COMPUTATIONAL FLUID DYNAMICS - COMPUTATIONAL GRIDS - GRID GENERATION (MATHEMATICS) - SUBSONIC FLOW - FINS - FUSELAGES - SUPERSONIC FLOW - Barger, Raymond L. - Adams, Mary S. - Krishnan, Ramki R.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19940032443
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The book is available for download in "texts" format, the size of the file-s is: 20.38 Mbs, the file-s for this book were downloaded 65 times, the file-s went public at Fri Oct 07 2016.
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