Flutter Failure Risk Assessment for Damage-Tolerant Composite Aircraft Structures

被引：11

作者：

Styuart, Andrey V. ^{[1
]}

Livne, Eli ^{[1
]}

Demasi, Luciano ^{[1
]}

Mor, Marat ^{[1
]}

机构：

[1] Univ Washington, Dept Aeronaut & Astronaut, Seattle, WA 98195 USA

来源：

AIAA JOURNAL | 2011年 / 49卷 / 03期

关键词：

AERODYNAMIC SHAPE SENSITIVITIES; AEROELASTIC ANALYSIS; OPTIMIZATION; DESIGN; SIMULATION;

D O I：

10.2514/1.J050862

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The quantitative assessment of the effects of damage and material degradation on the dynamic aeroelastic reliability of composite aircraft has become more challenging in recent years due to the increased use of composites in main structural components of passenger aircraft. This paper presents a method for quantifying the flutter reliability of aircraft composite structures in the presence of multiple uncertainties. Automated rapid simulation tools for predicting flutter speeds of composite airframes subject to multiple uncertainties serve a key role and are used in Monte Carlo simulations. A thorough discussion is presented of the flutter uncertainty of composite aircraft covering material degradation, damage, repair, and design and certification practices, as well as maintenance procedures. The effectiveness of the method and its potential are illustrated using a composite tail/rudder structure representing a typical passenger aircraft structure. Conclusions are drawn and recommendations for future work are made.

引用

页码：655 / 669

页数：15

共 50 条

[31] Corrosion risk assessment of aircraft structures
Liao, M
Komorowski, JP
[J]. PROBABILISTIC ASPECTS OF LIFE PREDICTION, 2004, 1450 : 183 - 198
[32] Use of microfasteners to produce damage tolerant composite structures
Partridge, Ivana K.
Hallett, Stephen R.
[J]. PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2016, 374 (2071):
[33] Damage tolerance of composite structures for large transport aircraft
Roudolff, F
Gädke, M
[J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2000, 4 (01): : 23 - 32
[34] Damage distribution of composite structures of a certain type aircraft
Deng J.
Chen L.
Lu S.
Hou Y.
Huang W.
Cheng X.
[J]. Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2024, 50 (03): : 920 - 930
[35] A damage-tolerant Ti-rich multiphase metallic-glass composite with hierarchically heterogeneous architecture
Lin, Shifeng
Zhu, Zhengwang
Liu, Zengqian
Ge, Shaofan
Liu, Dingming
Li, Hong
Li, Zhengkun
Fu, Huameng
Wang, Aimin
Zhang, Zhefeng
Zhang, Haifeng
Ritchie, Robert O.
[J]. COMPOSITES PART B-ENGINEERING, 2023, 263
[36] Damage identification and assessment in composite structures
Ostachowicz, Wieslaw M.
Wandowski, Tomasz
Malinowski, Pawel H.
Kudela, Pawel
[J]. STRUCTURAL HEALTH MONITORING - FROM SENSING TO DIAGNOSIS AND PROGNOSIS, 2017, 188 : 241 - 247
[37] Analysis of the adhesive failure in bonded composite repair of aircraft structures using modified damage zone theory
Bouanani, M. Fari
Benyahia, F.
Albedah, A.
Aid, A.
Bouiadjra, B. Bachir
Belhouari, M.
Achour, T.
[J]. MATERIALS & DESIGN, 2013, 50 : 433 - 439
[38] Damage, stiffness loss, and failure in composite structures
Chatterjee, SN
[J]. COMPOSITE STRUCTURES: THEORY AND PRACTICE, 2001, 1383 : 452 - 469
[39] Damage, stiffness loss, and failure in composite structures
Chatterjee, Sailendra N.
[J]. ASTM Special Technical Publication, 2000, (1383): : 452 - 469
[40] Microscale testing and modelling for damage tolerant composite materials and structures
Sorensen, Bent F.
[J]. 41ST RISO INTERNATIONAL SYMPOSIUM ON MATERIALS SCIENCE: MATERIALS AND DESIGN FOR NEXT GENERATION WIND TURBINE BLADES, 2020, 942

← 1 2 3 4 5 →