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| 报告编号 | NASA-CR-132575-4 |
| 来源ID | NTRS_Document_ID: 19760021134 |
| Arrow-wing supersonic cruise aircraft structural design concepts evaluation. Volume 4: Sections 15 through 21 | |
| Sakata, I. F.; Davis, G. W. | |
| 英文摘要 | The analyses performed to provide structural mass estimates for the arrow wing supersonic cruise aircraft are presented. To realize the full potential for structural mass reduction, a spectrum of approaches for the wing and fuselage primary structure design were investigated. The objective was: (1) to assess the relative merits of various structural arrangements, concepts, and materials; (2) to select the structural approach best suited for the Mach 2.7 environment; and (3) to provide construction details and structural mass estimates based on in-depth structural design studies. Production costs, propulsion-airframe integration, and advanced technology assessment are included. |
| 英文关键词 | ARROW WINGS STRUCTURAL DESIGN CRITERIA SUPERSONIC AIRCRAFT AIRCRAFT DESIGN AIRFRAMES COST ANALYSIS DESIGN ANALYSIS FUSELAGES PROPULSION SYSTEM CONFIGURATIONS STRUCTURAL MEMBERS TECHNOLOGY ASSESSMENT WEIGHT (MASS) WEIGHT REDUCTION |
| 出版年 | 1975 |
| 报告类型 | Technical Report |
| 语种 | 英语 |
| 国家 | 美国 |
| URL | http://hdl.handle.net/2060/19760021134 |
| 资源类型 | 科技报告 |
| 条目标识符 | http://119.78.100.177/qdio/handle/2XILL650/258586 |
| 推荐引用方式 GB/T 7714 | Sakata, I. F.,Davis, G. W.. Arrow-wing supersonic cruise aircraft structural design concepts evaluation. Volume 4: Sections 15 through 21,1975. |
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