Study on Airworthiness Requirements of Composite Aircraft Structure for Transport Category Aircraft in FAA-Reference-Cited by-同舟云学术

Study on Airworthiness Requirements of Composite Aircraft Structure for Transport Category Aircraft in FAA

Published:2011 Issue: Volume:17 Page:270-278
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Jian Xie,Yao Lu

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference11 articles.

1. J. T. Quinlivan, J.A. Kent, and D. R. Wilson, “NASA-ACEE/Boeing 737 Graphite/Epoxy Horizontal Stabilizer Service”, 9th DoD/NASA Conference On Fibrous Composite in Structural Design, 1991.

2. J. E. McCarty, R.W. Johnson, and D. R. Wilson, “737 Graphite/Epoxy Horizontal Stabilizer Certification”, AIAA Paper 82-0745.

3. K. H. Schreiber and J. T. Quinlivan “The Boeing 777 Empenage”, Presented at ICCM-9 Madrid 1993.

4. J. Takai, et.al, “CFRP Horizontal Stabilizer Development Test Program”, Presented at ICCM-9, Madrid 1993.

5. T. Ford, “ATR Composite Wing”, Aircraft Engineering, September/October 1993 pp 22-24.

Cited by 15 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Does hygrothermal degradation of Mode I fatigue delamination resistance in carbon fibre reinforced polymer laminates depend on the ageing conditions?;Composite Structures;2024-08

2. Strategies towards a more sustainable aviation: A systematic review;Progress in Aerospace Sciences;2023-02

3. A Study on Aircraft Structure and Application of Static Force;1;2022-09-01

4. Effect of Patch Repair on the Physical and Mechanical Properties of Carbon Bidirectional Reinforced Composites;Iranian Journal of Science and Technology, Transactions of Mechanical Engineering;2022-07-18

5. Evaluation of test methods and face-sheet thickness effects in damage tolerance assessment of composite sandwich plates;Journal of Sandwich Structures & Materials;2021-08-05