Finite element analysis of S aircraft skin stretch forming

Jin Quan Han; Min Wan; Hai Xia Jin; Hui Wu

Finite element analysis of S aircraft skin stretch forming

Jin Quan Han
, Min Wan^*
, Hai Xia Jin
, Hui Wu

^*Corresponding author for this work

School of Mechanical Engineering and Automation

Beihang University
China Aviation Industry Corporation

Research output: Contribution to conference › Paper › peer-review

1 Scopus citations

Abstract

S aircraft skin, which is one kind of complex skins used more and more on modern planes, is difficult in processing due to its complicacy in shape. Therefore the stretching of S skin is simulated with finite element method in order to obtain the reasonable parameters in stretching. The elongation percentages are used instead of stretching coefficient to gain the jaw path as controlling parameters when simulation. Several groups of results achieved with different parameters are estimated with forming limited diagram (FLD) and springback.

Original language	English
Pages	1053-1058
Number of pages	6
State	Published - 2008
Event	9th International Conference on Technology of Plasticity, ICTP 2008 - Gyeongju, Korea, Republic of Duration: 7 Sep 2008 → 11 Sep 2008

Conference

Conference	9th International Conference on Technology of Plasticity, ICTP 2008
Country/Territory	Korea, Republic of
City	Gyeongju
Period	7/09/08 → 11/09/08

Cite this

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title = "Finite element analysis of S aircraft skin stretch forming",

abstract = "S aircraft skin, which is one kind of complex skins used more and more on modern planes, is difficult in processing due to its complicacy in shape. Therefore the stretching of S skin is simulated with finite element method in order to obtain the reasonable parameters in stretching. The elongation percentages are used instead of stretching coefficient to gain the jaw path as controlling parameters when simulation. Several groups of results achieved with different parameters are estimated with forming limited diagram (FLD) and springback.",

author = "Han, \{Jin Quan\} and Min Wan and Jin, \{Hai Xia\} and Hui Wu",

year = "2008",

language = "英语",

pages = "1053--1058",

note = "9th International Conference on Technology of Plasticity, ICTP 2008 ; Conference date: 07-09-2008 Through 11-09-2008",

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TY - CONF

T1 - Finite element analysis of S aircraft skin stretch forming

AU - Han, Jin Quan

AU - Wan, Min

AU - Jin, Hai Xia

AU - Wu, Hui

PY - 2008

Y1 - 2008

N2 - S aircraft skin, which is one kind of complex skins used more and more on modern planes, is difficult in processing due to its complicacy in shape. Therefore the stretching of S skin is simulated with finite element method in order to obtain the reasonable parameters in stretching. The elongation percentages are used instead of stretching coefficient to gain the jaw path as controlling parameters when simulation. Several groups of results achieved with different parameters are estimated with forming limited diagram (FLD) and springback.

AB - S aircraft skin, which is one kind of complex skins used more and more on modern planes, is difficult in processing due to its complicacy in shape. Therefore the stretching of S skin is simulated with finite element method in order to obtain the reasonable parameters in stretching. The elongation percentages are used instead of stretching coefficient to gain the jaw path as controlling parameters when simulation. Several groups of results achieved with different parameters are estimated with forming limited diagram (FLD) and springback.

UR - https://www.scopus.com/pages/publications/77950971489

M3 - 论文

AN - SCOPUS:77950971489

SP - 1053

EP - 1058

T2 - 9th International Conference on Technology of Plasticity, ICTP 2008

Y2 - 7 September 2008 through 11 September 2008

ER -

Finite element analysis of S aircraft skin stretch forming

Abstract

Conference

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