Approximate function for fatigue crack propagation in a design optimisation procedure for fibre metal laminates

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

1 Citation (Scopus)

Original language	Undefined/Unknown
Title of host publication	Proc. 29th Congress of the International Council of the Aeronautical Sciences
Editors	s.n.
Place of Publication	St. Petersburg, Russia
Publisher	ICAS
Pages	1-6
Number of pages	6
Publication status	Published - 2014
Event	29th Congress of the International Council of the Aeronautical Sciences - St. Petersburg, Russia Duration: 7 Sept 2014 → 12 Sept 2014

Name
Publisher	ICAS

Conference	29th Congress of the International Council of the Aeronautical Sciences
Period	7/09/14 → 12/09/14

Keywords

@inproceedings{9ff6c70b31784f0bb2aa4c6c2c23ecb8,

title = "Approximate function for fatigue crack propagation in a design optimisation procedure for fibre metal laminates",

keywords = "Conf.proc. > 3 pag",

author = "I Sen and RC Alderliesten and R Benedictus",

year = "2014",

language = "Undefined/Unknown",

publisher = "ICAS",

pages = "1--6",

editor = "s.n.",

booktitle = "Proc. 29th Congress of the International Council of the Aeronautical Sciences",

note = "29th Congress of the International Council of the Aeronautical Sciences ; Conference date: 07-09-2014 Through 12-09-2014",

}

Sen, I, Alderliesten, RC & Benedictus, R 2014, Approximate function for fatigue crack propagation in a design optimisation procedure for fibre metal laminates. in s.n. (ed.), Proc. 29th Congress of the International Council of the Aeronautical Sciences. ICAS, St. Petersburg, Russia, pp. 1-6, 29th Congress of the International Council of the Aeronautical Sciences, 7/09/14.

Approximate function for fatigue crack propagation in a design optimisation procedure for fibre metal laminates. / Sen, I; Alderliesten, RC ; Benedictus, R.
Proc. 29th Congress of the International Council of the Aeronautical Sciences. ed. / s.n. St. Petersburg, Russia: ICAS, 2014. p. 1-6.

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

TY - GEN

T1 - Approximate function for fatigue crack propagation in a design optimisation procedure for fibre metal laminates

AU - Sen, I

AU - Alderliesten, RC

AU - Benedictus, R

PY - 2014

Y1 - 2014

KW - Conf.proc. > 3 pag

M3 - Conference contribution

SP - 1

EP - 6

BT - Proc. 29th Congress of the International Council of the Aeronautical Sciences

A2 - s.n., null

PB - ICAS

CY - St. Petersburg, Russia

T2 - 29th Congress of the International Council of the Aeronautical Sciences

Y2 - 7 September 2014 through 12 September 2014

ER -