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Boron-Epoxy Wing Skins F-100D Aircraft Structural Design and Analysis.

机译：Boron-Epoxy Wing skins F-100D飞机结构设计与分析。

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This document constitutes the final report on the structural analysis and design of boron-epoxy wing skins. The design and fabrication of boron composite laminate skins are intended to replace the upper and lower structural covers of the F-100D wing. This report presents the final design of these boron-epoxy wing skins and the material properties and structural analysis. Structural optimization and analysis are presented. (P.S.-PL)

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作者
Stotler, C. L.; Van Putten, D. J.; Dickerson, E. O.;
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年度 1971
页码 1-114
总页数 114
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Airplane panels; Composite materials; Sweptback wings; Mechanical drawings; Reinforced plastics; Boron; Epoxy resins; Laminated plastics; Jet fighters; Design; Skin(Structural member); Boron reinforced plastics; Fiber composites; F-100 aircraft;

机译：飞机板;复合材料;后掠翼;机械图纸;增强塑料;硼;环氧树脂;层压塑料;喷气式战斗机;设计;表皮（结构构件）;硼增强塑料;纤维复合材料; F-100飞机;

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1. Structural Design and Optimization of an Aircraft Morphing Wing: Composite Skin [J] . Michaud Francois, Dalir Hamid, Joncas Simon Journal of Aircraft . 2018,第1期

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2. The development of a preliminary structural design optimization method of an aircraft wing-box skin-stringer panels [J] . Sridhar Chintapalli, Mostafa S.A. Elsayed, Ramin Sedaghati, Aerospace science and technology . 2010,第3期

机译：飞机机翼箱纵梁面板初步结构设计优化方法的开发
3. Design Criteria for Variable Camber Compliant Wing Aircraft Morphing Wing Skin [J] . You Hangil, Kim Seongik, Yun Gun Jin AIAA Journal . 2020,第2期

机译：可变弧度的机翼飞机变形机翼蒙皮的设计标准
4. Structural analysis of the aircraft wing box with a splice joint in the bottom skin [C] . Anand H.R., Udupa N.G.S., Girish K.E. National Conference on Challenges in Research Technology in the Coming Decades . 2014

机译：底部皮肤中带接头的飞机翼盒的结构分析
5. Optimal structural design of a morphing aircraft wing. [D] . Bharti, Smita. 2007

机译：变形机翼的最佳结构设计。
6. An Improved Gaussian Mixture Model for Damage Propagation Monitoring of an Aircraft Wing Spar under Changing Structural Boundary Conditions [O] . Lei Qiu, Shenfang Yuan, Hanfei Mei, 2016

机译：改进的高斯混合模型用于在变化的结构边界条件下监测机翼翼梁的损伤传播
7. Design of Aircraft Structures - Structural Design of Carbon Fiber Composite Wing for the SARAS Civil Transport Aircraft [O] . Murthy Sridhara S 2010

机译：飞机结构设计-SARAS民用运输机碳纤维复合材料机翼的结构设计
8. Boron-Epoxy Wing Skins F-100D Aircraft Structural Design and Analysis. [R] . Stotler, C. L., Van Putten, D. J., Dickerson, E. O. 1971

机译：Boron-Epoxy Wing skins F-100D飞机结构设计与分析。

Boron-Epoxy Wing Skins F-100D Aircraft Structural Design and Analysis.

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