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"ZHAI XINKANG"
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"ZHAI XINKANG"
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Dynamic monitoring method of measurement data in fatigue test of aircraft structure
by
ZHAI XINKANG
Year of Publication
09.04.2019
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Determining method for loading frequency of airplane structure fatigue test
by
ZHAI XINKANG
Year of Publication
09.04.2019
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Device for testing friction force of counter weight steel wire rope in airplane structure test and estimation method
by
ZHAI XINKANG
Year of Publication
05.04.2019
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Steel wire rope friction coefficient test device and estimation method
by
ZHAI XINKANG
Year of Publication
05.04.2019
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Method for determining dispersion coefficient of theoretical value of aircraft structure crack propagation life
by
ZHAI XINKANG
,
TIAN XIAOXING
Year of Publication
18.05.2021
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Testing method for static strength of airplane structure
by
ZHAI XINKANG
,
TIAN XIAOXING
Year of Publication
11.05.2021
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Aircraft structure failure mode analysis method based on fracture analysis
by
ZHAI XINKANG
,
TIAN XIAOXING
Year of Publication
07.05.2021
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Method for determining theoretical value dispersion coefficient of crack forming life of aircraft structure
by
ZHAI XINKANG
,
TIAN XIAOXING
Year of Publication
23.04.2021
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Rationality determination method for structural parameter matching of integral reinforced wallboard of aircraft
by
ZHAI XINKANG
,
TIAN XIAOXING
Year of Publication
23.04.2021
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Method for determining accuracy of strain measurement value in aircraft structural strength test
by
ZHAI XINKANG
,
TIAN XIAOXING
Year of Publication
06.04.2021
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Strain theoretical value obtaining method and device based on finite element model
by
ZHAI XINKANG
,
TIAN XIAOXING
Year of Publication
19.05.2020
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Method for determining airplane structure fatigue crack propagation track
by
ZHAI XINKANG
,
TIAN XIAOXING
Year of Publication
15.05.2020
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Method and device for determining position of airplane structure fatigue crack arrest hole
by
ZHAI XINKANG
,
TIAN XIAOXING
Year of Publication
24.04.2020
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Method and device for predicting fatigue crack propagation direction of aircraft structure
by
ZHAI XINKANG
,
TIAN XIAOXING
Year of Publication
27.03.2020
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Method for calculating dimensionless stress intensity factor of integral wing spar of airplane
by
ZHANG ZHE
,
ZHAI XINKANG
,
TIAN XIAOXING
Year of Publication
21.04.2020
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Detail fatigue rating (DFR) reference value determination method for folding direction connection structure stress in different phases
by
ZHAI XINKANG
,
ZHANG YANJUN
,
LEI XIAOXIN
,
LI XIAOPENG
Year of Publication
08.04.2015
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Fatigue test clamp for large opening of spar
by
ZHAI XINKANG
,
ZHANG YANJUN
,
ZHAO TIANJIAO
,
LI XIAOPENG
,
WANG FENG
Year of Publication
14.05.2021
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Aircraft structure test piece bending preventing and measuring device and measuring method thereof
by
WANG XINBEI
,
ZHAI XINKANG
,
QIN JIANBO
Year of Publication
12.10.2016
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Anti-bending design method of airplane single lap structure test article
by
ZHAI XINKANG
,
NING YU
,
WANG FENG
Year of Publication
12.10.2016
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Method for designing fatigue life of aircraft bolts
by
ZHAI XINKANG
,
WANG XINBO
,
ZHANG YANJUN
Year of Publication
22.01.2014
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