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Automatic Procedures For Computing Complete Configuration Geometry From Individual Component Descriptions by Raymond L. Barger
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1NASA Technical Reports Server (NTRS) 19940032435: Automatic Procedures For Computing Complete Configuration Geometry From Individual Component Descriptions
By NASA Technical Reports Server (NTRS)
Procedures are derived for developing a complete airplane surface geometry starting from component descriptions. The procedures involve locating the intersection lines of adjacent components and omitting any regions for which part of one surface lies within the other. The geometry files utilize the wave-drag (Harris) format, and output files are written in Hess format. Two algorithms are used: one, if both intersecting surfaces have airfoil cross sections; the other, if one of the surfaces has circular cross sections. Some sample results in graphical form are included.
“NASA Technical Reports Server (NTRS) 19940032435: Automatic Procedures For Computing Complete Configuration Geometry From Individual Component Descriptions” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19940032435: Automatic Procedures For Computing Complete Configuration Geometry From Individual Component Descriptions
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19940032435: Automatic Procedures For Computing Complete Configuration Geometry From Individual Component Descriptions” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - AIRCRAFT CONFIGURATIONS - COMPUTATIONAL GEOMETRY - COMPUTATIONAL GRIDS - GRID GENERATION (MATHEMATICS) - SURFACE GEOMETRY - AERODYNAMIC CONFIGURATIONS - AIRFOIL PROFILES - ALGORITHMS - Barger, Raymond L. - Adams, Mary S.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19940032435
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The book is available for download in "texts" format, the size of the file-s is: 12.40 Mbs, the file-s for this book were downloaded 56 times, the file-s went public at Fri Oct 07 2016.
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