| タイトル | A Study of Vehicle Structural Layouts in Post-WWII Aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040058112 |
| 著者（英） | Samareh, Jamshid A.; Sensmeier, Mark D. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2004-01-01 |
| 言語 | eng |
| 内容記述 | In this paper, results of a study of structural layouts of post-WWII aircraft are presented. This study was undertaken to provide the background information necessary to determine typical layouts, design practices, and industry trends in aircraft structural design. Design decisions are often predicated not on performance-related criteria, but rather on such factors as manufacturability, maintenance access, and of course cost. For this reason, a thorough understanding of current best practices in the industry is required as an input for the design optimization process. To determine these best practices and industry trends, a large number of aircraft structural cutaway illustrations were analyzed for five different aircraft categories (commercial transport jets, business jets, combat jet aircraft, single engine propeller aircraft, and twin-engine propeller aircraft). Several aspects of wing design and fuselage design characteristics are presented here for the commercial transport and combat aircraft categories. A great deal of commonality was observed for transport structure designs over a range of eras and manufacturers. A much higher degree of variability in structural designs was observed for the combat aircraft, though some discernable trends were observed as well. |
| NASA分類 | Aircraft Design, Testing and Performance |
| レポートNO | AIAA Paper 2004-1624 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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