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Present capabilities and future requirements for computer-aided geometric modeling in the design and manufacture of gas turbine (1984)

Caille, E. ; Hoffman, A. ; Propen, M.

In: CASI

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Publication Date: 2006-04-09

Description: Gas turbine engine design requires the ability to rapidly develop complex structures which are subject to severe thermal and mechanical operating loads. As in all facets of the aerospace industry, engine designs are constantly driving towards increased performance, higher temperatures, higher speeds, and lower weight. The ability to address such requirements in a relatively short time frame has resulted in a major thrust towards integrated design/analysis/manufacturing systems. These computer driven graphics systems represent a unique challenge, with major payback opportunities if properly conceived, implemented, and applied.

Keywords: COMPUTER PROGRAMMING AND SOFTWARE

Type: NASA. Langley Research Center Computer-Aided Geometry Modeling; p 321-325

Format: text

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