THE EVALUATION OF THEORETICAL CRITICAL COMPRESSION IN SANDWICH PLATES

被引：22

作者：

GOODIER, JN

NEOU, IM

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1951年 / 18卷 / 10期

关键词：

D O I：

10.2514/8.2071

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：649 / &

共 11 条

[1]

BIJLAARD PP, 1947, P ROYAL NETHERLANDS, V50

[2]

COX HL, 1945, ARC2125 TECHN REP R

[3]

FLUGGE W, 1947, ONERA421R10110OR RAP

[4]

GOODIER JN, 1946, J APPL MECH-T ASME, V13, pA253

[5]

Gough GS, 1940, J ROYAL AERONAUTICAL, V44, P12

[6] THE BUCKLING OF SANDWICH-TYPE PANELS [J].

HOFF, NJ ;

MAUTNER, SE .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1945, 12 (03) :285-297

[7] BENDING AND BUCKLING OF SANDWICH BEAMS [J].

HOFF, NJ ;

MAUTNER, SE .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1948, 15 (12) :707-720

[8]

MARCH HW, 1948, FOREST PRODUCTS LABO, V1583

[9]

NEUBER H, 1948, TTS964RE REP

[10] COLUMN CHARACTERISTICS OF SANDWICH PANELS HAVING HONEYCOMB CORES [J].

TROXELL, WW ;

ENGEL, HC .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1947, 14 (07) :413-421