IMPACT BUCKLING OF A THIN BAR

被引：56

作者：

LINDBERG, HE

机构：

来源：

JOURNAL OF APPLIED MECHANICS | 1965年 / 32卷 / 02期

关键词：

D O I：

10.1115/1.3625801

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

页码：315 / &

共 17 条

[1]

ABRAHAMSON GR, 1964, WLTDR6422 AIR FORC W

[2] BUCKLING OF STRUTS UNDER DYNAMIC LOADING [J].

DAVIDSON, JF .

[3]

ELLIS AT, 1963, J APPLIED MECHANIC E, V30, P51

[4] SHOCK WAVE COMPRESSION OF HARDENED AND ANNEALED 2024 ALUMINUM [J].

FOWLES, GR .

[5] COLUMN BEHAVIOR UNDER CONDITIONS OF IMPACT [J].

GERARD, G ;

BECKER, H .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (01) :58-&

[6]

HOFF NJ, 1951, J APPL MECH-T ASME, V18, P68

[7]

HOUSNER GW, 1962, J ENGINEERING ME OCT, P41

[8]

LAVRENTEV MA, 1949, DOKL AKAD NAUK SSSR+, V64, P779

[9]

Lindberg H.E., 1964, J APPL MECH, V31, P267

[10] FINITE ELASTIC WAVE PROPAGATION IN RUBBER [J].

MASON, P .