Supersonic flutter analysis of stiffened isotropic and anisotropic panels

被引：8

|

作者：

Lee, DM

Lee, I

机构：

[1] Department of Aerospace Engineering, Korea Adv. Inst. Sci. and Technol., Yusong-Gu, Taejon 305-701, 373-1, Kusong-Dong

来源：

AIAA JOURNAL | 1996年 / 34卷 / 03期

关键词：

D O I：

10.2514/3.60020

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

收藏

页码：637 / 639

页数：3

相关论文

共 50 条

[11] SUPERSONIC FLUTTER OF LAMINATED CURVED PANELS
GANAPATHI, M
VARADAN, TK
DEFENCE SCIENCE JOURNAL, 1995, 45 (02) : 147 - 159
[12] Supersonic flutter analysis of stiffened laminated plates subject to thermal load
Lee, I
Lee, DM
Oh, IK
JOURNAL OF SOUND AND VIBRATION, 1999, 224 (01) : 49 - 67
[13] Numerical Analysis of Dynamic Stability of Flutter Panels in Supersonic Flow
Deng, Jian
Liu, Airong
Zhong, Zilin
INTERNATIONAL JOURNAL OF STRUCTURAL STABILITY AND DYNAMICS, 2024,
[14] Flutter analysis of stiffened laminated composite plates and shells in supersonic flow
Liao, Chung-Li, 1897, (31):
[15] Finite element supersonic flutter analysis of low aspect ratio stiffened wing
Faroughi, Shirko
Malekzadeh, Kramet
Mirzaee, Ieraje
JOURNAL OF VIBRATION AND CONTROL, 2013, 19 (14) : 2187 - 2198
[16] FLUTTER OF FLAT PANELS AT LOW SUPERSONIC SPEEDS
FAURE, G
RECHERCHE AEROSPATIALE, 1967, (118): : 53 - &
[17] FLUTTER ANALYSIS OF STIFFENED LAMINATED COMPOSITE PLATES AND SHELLS IN SUPERSONIC-FLOW
LIAO, CL
SUN, YW
AIAA JOURNAL, 1993, 31 (10) : 1897 - 1905
[18] Finite element supersonic flutter analysis of skewed and cracked composite panels
Pidaparti, RMV
Chang, CC
COMPUTERS & STRUCTURES, 1998, 69 (02) : 265 - 270
[19] ON FLUTTER OF MULTIBAY PANELS AT LOW SUPERSONIC SPEEDS
DOWELL, EH
AIAA JOURNAL, 1967, 5 (05) : 1032 - &
[20] FINITE-ELEMENT ANALYSIS OF SUPERSONIC FLUTTER OF MULTIBAY COMPOSITE PANELS
SHIAU, LC
CHANG, JT
COMPUTERS & STRUCTURES, 1991, 39 (3-4) : 269 - 276

← 1 2 3 4 5 →