FRACTURE BEHAVIOR OF BORON FILAMENTS

被引：25

作者：

LAYDEN, GK ^{[1
]}

机构：

[1] UNITED AIRCRAFT RES LABS,E HARTFORD,CT 06108

来源：

关键词：

D O I：

10.1007/BF00754893

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

引用

页码：1581 / 1589

页数：9

共 13 条

ADLER, RPI ;

HAMMOND, ML .

[2]

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[3]

BOURDEAU RG, 1968, G1105502 UN AIRCR RE

[4]

DIEFENDORF RJ, 1971, AFMLTR70287 TECHN RE

[5] ON SHAPE AND SIZE OF FRACTURE ZONES ON GLASS FRACTURE SURFACES [J].

JOHNSON, JW ;

HOLLOWAY, DG .

PHILOSOPHICAL MAGAZINE, 1966, 14 (130) :731-&

[6]

KREIDER KG, 1972, STP497 ASTM COMP MAT, P539

[7]

LASDAY AH, 1966, ADV FIBROUS REINFORC, V10

[8]

LINE LE, 1969, HDB FIBERGLASS ADV P

[9]

PREWO KM, TO BE PUBLISHED

[10]

SCHARDIN H, 1959, FRACTURE