.245
a	Presentation and analysis of results of an unsteady transonic wind tunnel test on a semi-span delta wing model, oscillating in pitch.
h	Book
.100
a	Geurts E.G.M.
.005
a	00000000000000
.260
a	Amsterdam: National Aerospace Laboratory NLR, 1995.
b
c	2000
.084
a	NLR Pro
.300
a	16 hlm.
b	gamb., 29 cm.
c	16 hlm.; gamb., 29 cm.
.490
a	Nationaal Lucht-en Ruimtevaartlaboratorium; NLR TP
.336
a	Book