FLUTTER ANALYSIS OF THIN CRACKED PANELS USING THE FINITE-ELEMENT METHOD

被引：17

作者：

CHEN, WH

LIN, HC

机构：

[1] Natl Tsinghua Univ, Dep of Power, Mechanical Engineering, Hsinchu,, Taiwan, Natl Tsinghua Univ, Dep of Power Mechanical Engineering, Hsinchu, Taiwan

来源：

AIAA JOURNAL | 1985年 / 23卷 / 05期

关键词：

D O I：

10.2514/3.8986

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：795 / 801

页数：7

共 24 条

[1] PISTON THEORY - A NEW AERODYNAMIC TOOL FOR THE AEROELASTICIAN [J].

ASHLEY, H ;

ZARTARIAN, G .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (12) :1109-1118

[2]

Barsoum R. S., 1971, International Journal for Numerical Methods in Engineering, V3, P63, DOI 10.1002/nme.1620030110

[3] ON ELASTODYNAMIC FRACTURE-MECHANICS ANALYSIS OF BI-MATERIAL STRUCTURES USING FINITE-ELEMENT METHOD [J].

CHEN, WH ;

WU, CW .

ENGINEERING FRACTURE MECHANICS, 1981, 15 (1-2) :155-168

[4] A HYBRID-DISPLACEMENT FINITE-ELEMENT MODEL FOR THE BENDING ANALYSIS OF THIN CRACKED PLATES [J].

CHEN, WH ;

CHEN, PY .

INTERNATIONAL JOURNAL OF FRACTURE, 1984, 24 (02) :83-106

[5]

CHEN WH, 1981, ENG STRUCT, V3, P249

[6]

CHEN WH, 1983, APR P ROC ROK JOINT, P217

[7]

CHEN WH, 1980, J CHINESE SOC MECH E, V1, P21

[8]

CHEN WH, 1983, ENG FRACTURE MECHANI, V17, P133

[9]

CHEN WH, 1981, 5TH INT C FRACT CANN

[10] NONLINEAR OSCILLATIONS OF A FLUTTERING PLATE [J].

DOWELL, EH .

AIAA JOURNAL, 1966, 4 (07) :1267-&

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