NONLINEAR ANALYSIS OF SHELLS OF REVOLUTION BY MATRIX DISPLACEMENT METHOD

被引：35

作者：

STRICKLIN, JA

HAISLER, WE

MACDOUGALL, HR

STEBBINS, FJ

机构：

来源：

AIAA JOURNAL | 1968年 / 6卷 / 12期

关键词：

D O I：

10.2514/3.4987

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：2306 / +

页数：1

共 15 条

[1]

AMBARTSUMIAN SA, 1964, TTF118 NASA, P53

[2]

GALLAGHER RH, 1965, D7218933005 BELL AER

[3] ANALYSIS OF AXISYMMETRICAL SHELLS BY THE DIRECT STIFFNESS METHOD [J].

GRAFTON, PE ;

STROME, DR .

AIAA JOURNAL, 1963, 1 (10) :2342-2347

[4] RIGID-BODY DISPLACEMENTS OF CURVED ELEMENTS IN ANALYSIS OF SHELLS BY MATRIX-DISPLACEMENT METHOD [J].

HAISLER, WE ;

STRICKLI.JA .

AIAA JOURNAL, 1967, 5 (08) :1525-&

[5] DIRECT STIFFNESS METHOD ANALYSIS OF SHELLS OF REVOLUTION UTILIZING CURVED ELEMENTS [J].

JONES, RE ;

STROME, DR .

AIAA JOURNAL, 1966, 4 (09) :1519-&

[6]

LANGHAAR HL, 1962, ENERGY METHODS APPLI, P187

[7]

LU ZA, 1964, CR37 NASA

[8] CONICAL SEGMENT METHOD FOR ANALYZING OPEN CROWN SHELLS OF REVOLUTION FOR EDGE LOADING [J].

MEYER, RR ;

HARMON, MB .

AIAA JOURNAL, 1963, 1 (04) :886-891

[9] COMPUTATION OF STRESS RESULTANTS IN FINITE ELEMENT ANALYSIS [J].

NAVARATNA, DR .

AIAA JOURNAL, 1966, 4 (11) :2058-+

[10]

NAVARATNA DR, 1967, 8 AIAAASME STRUCT ST, P175

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