Fatigue, residual strength and non-destructive tests of an aging aircraft's wing detail

Keijo Koski; Aslak Siljander; Mika Bäckström; Sauli Liukkonen; Juha Juntunen; Matti Sarkimo; Kari Lahdenperä; J. Tikka; R. Lahtinen

doi:10.1016/j.ijfatigue.2008.05.015

Fatigue, residual strength and non-destructive tests of an aging aircraft's wing detail

Keijo Koski (Corresponding Author), Aslak Siljander, Mika Bäckström, Sauli Liukkonen, Juha Juntunen, Matti Sarkimo, Kari Lahdenperä, J. Tikka, R. Lahtinen

Research output: Contribution to journal › Article › Scientific › peer-review

5 Citations (Scopus)

Abstract

This study concentrates on fatigue, residual strength and non-destructive tests of an aging aircraft’s wing detail of the Finnish Air Force’s Hawk Mk.51 jet trainer. The studied detail was the integral stiffener with a drain hole near the wing root. Fatigue tests were deemed necessary to verify experimentally the analytically observed short fatigue life, significant crack growth rates and eventually to re-assess the detail’s inspection period for the fleet jets. The results of the study have been utilized e.g. at the complementary type approval accomplished for the Finnish Air Force’s Hawk.

Original language	English
Pages (from-to)	1089-1094
Number of pages	6
Journal	International Journal of Fatigue
Volume	31
Issue number	6
DOIs	https://doi.org/10.1016/j.ijfatigue.2008.05.015
Publication status	Published - 2009
MoE publication type	A1 Journal article-refereed
Event	International Conference on Damage Tolerance of Aircraft Structures, DTAS2007 - Delft, Netherlands Duration: 25 Sept 2007 → 28 Sept 2007

Keywords

jet trainer
drain hole
wing
fatigue test
residual strength test
non-destructive test

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10.1016/j.ijfatigue.2008.05.015

Cite this

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title = "Fatigue, residual strength and non-destructive tests of an aging aircraft's wing detail",

abstract = "This study concentrates on fatigue, residual strength and non-destructive tests of an aging aircraft{\textquoteright}s wing detail of the Finnish Air Force{\textquoteright}s Hawk Mk.51 jet trainer. The studied detail was the integral stiffener with a drain hole near the wing root. Fatigue tests were deemed necessary to verify experimentally the analytically observed short fatigue life, significant crack growth rates and eventually to re-assess the detail{\textquoteright}s inspection period for the fleet jets. The results of the study have been utilized e.g. at the complementary type approval accomplished for the Finnish Air Force{\textquoteright}s Hawk.",

keywords = "jet trainer, drain hole, wing, fatigue test, residual strength test, non-destructive test",

author = "Keijo Koski and Aslak Siljander and Mika B{\"a}ckstr{\"o}m and Sauli Liukkonen and Juha Juntunen and Matti Sarkimo and Kari Lahdenper{\"a} and J. Tikka and R. Lahtinen",

year = "2009",

doi = "10.1016/j.ijfatigue.2008.05.015",

language = "English",

volume = "31",

pages = "1089--1094",

journal = "International Journal of Fatigue",

issn = "0142-1123",

publisher = "Elsevier",

number = "6",

note = "International Conference on Damage Tolerance of Aircraft Structures, DTAS2007 ; Conference date: 25-09-2007 Through 28-09-2007",

}

TY - JOUR

T1 - Fatigue, residual strength and non-destructive tests of an aging aircraft's wing detail

AU - Koski, Keijo

AU - Siljander, Aslak

AU - Bäckström, Mika

AU - Liukkonen, Sauli

AU - Juntunen, Juha

AU - Sarkimo, Matti

AU - Lahdenperä, Kari

AU - Tikka, J.

AU - Lahtinen, R.

PY - 2009

Y1 - 2009

N2 - This study concentrates on fatigue, residual strength and non-destructive tests of an aging aircraft’s wing detail of the Finnish Air Force’s Hawk Mk.51 jet trainer. The studied detail was the integral stiffener with a drain hole near the wing root. Fatigue tests were deemed necessary to verify experimentally the analytically observed short fatigue life, significant crack growth rates and eventually to re-assess the detail’s inspection period for the fleet jets. The results of the study have been utilized e.g. at the complementary type approval accomplished for the Finnish Air Force’s Hawk.

AB - This study concentrates on fatigue, residual strength and non-destructive tests of an aging aircraft’s wing detail of the Finnish Air Force’s Hawk Mk.51 jet trainer. The studied detail was the integral stiffener with a drain hole near the wing root. Fatigue tests were deemed necessary to verify experimentally the analytically observed short fatigue life, significant crack growth rates and eventually to re-assess the detail’s inspection period for the fleet jets. The results of the study have been utilized e.g. at the complementary type approval accomplished for the Finnish Air Force’s Hawk.

KW - jet trainer

KW - drain hole

KW - wing

KW - fatigue test

KW - residual strength test

KW - non-destructive test

U2 - 10.1016/j.ijfatigue.2008.05.015

DO - 10.1016/j.ijfatigue.2008.05.015

M3 - Article

SN - 0142-1123

VL - 31

SP - 1089

EP - 1094

JO - International Journal of Fatigue

JF - International Journal of Fatigue

IS - 6

T2 - International Conference on Damage Tolerance of Aircraft Structures, DTAS2007

Y2 - 25 September 2007 through 28 September 2007

ER -

Fatigue, residual strength and non-destructive tests of an aging aircraft's wing detail

Abstract

Keywords

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