.245
a	Impact damage prediction and failure analysis of heavily loaded, blade-stiffened composite wing panels, by J.F.M Wiggenraad, X.Zhang and G.A.O Davies.
h	Book
.100
a	Wiggenraad J.F.M.
.005
a	00000000000000
.260
a	Amsterdam: National Aerospace Laboratory NLR, 1998.
b
c	2000
.084
a	R 336.598 2 Ban
.300
a	44 hlm.
b	gamb., tab., 29 cm.
c	44 hlm.; gamb., tab., 29 cm.
.490
a	Nationaal Lucht-en Ruimtevaartlaboratorium; NLR 98
.336
a	Book