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¹Ú»ç
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2019.8
|
±èÁ¤È¯
|
A study on the optimization of the gyro structure considering the time-lagging thermoelastic dissipation
|
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2018.8
|
ÀÓÁ¤¼ö
|
Analysis of effective properties in smart multilayered plates in thermal environment and supersonic flow
|
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|
2017.8
|
ÀÓÅ°æ
|
Temperature-dependent shear correction factors for thermal-structural stability of step-wise FGM panel with micromechanical properties
|
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|
2017.2
|
°¼®Çö
|
Vibration and Buckling Analysis of Multifunctional Antenna Structures with Thermoelastic Characteristics
|
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|
2016.2
|
ÀÌ¿µÈÆ
|
Thermo-elastic analysis of structurally damped functionally graded plate with micro-mechanical properties
|
¹Ú»ç
|
2015.2
|
ÀÌâ¿
|
Active Flutter Control of Multifunctional Skin Antenna Structures considering Aerothermoelastic Characteristics
|
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|
2015.2
|
¹è¼®ÀÎ
|
Thermal buckling analysis of functionally graded plates considering neutral surface and homogenization scheme
|
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|
2014.8
|
±èÁ¤È¯
|
Mass and stiffness deviation effecton micro ring with thermoelastic damping
|
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|
2014.2
|
°¼®ÁÖ
|
Effects on Thermo-Elastic Damping of Micro-Ring Structure with Arbitrarily Attached Masses
|
¼®»ç
|
2011.8
|
À¯±¤±Ô
|
Analysis
and Optimal Design of Smart Skin Structure under Thermal
Effect
|
¼®»ç
|
2011.8
|
ÃÖ¼º¿
|
Natural
Frequency Split of Resonator Gyro Structures with Imperfection
|
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|
2011.8
|
Á¤À¯¿¬
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Aeroelastic
Study on a Folding Wing Structure in Subsonic Flow
|
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|
2008.2
|
ÀÌ»ó·¡
|
Non-linear Transient Response of Functionally Graded Panels Subjected to Thermal
and Blast Load in Supersonic Flow
|
¼®»ç
|
2007.2
|
¼Õ±âÁÖ
|
Thermal
Post-Buckling and Flutter Analyses of Functionally Graded
Panels in Supersonic Airflows
|
¹Ú»ç
|
2006.8
|
¹ÚÀç»ó
|
Design
and Aeroelastic Analysis of Active Twist Rotor Blades
Incorporating Single Crystal Piezoelectric Fiber Composite
Actuators
|
¹Ú»ç
|
2006.2
|
³ª°æ¼ö
|
Optimal
Design Functionally Graded Composite Plates Considering
Stress and Critcal Temperature
|
¼®»ç
|
2005.2
|
°º´±Ç
|
Optimal
Design of Smart Skin Using Genetic Algorithm
|
¼®»ç
|
2005.2
|
ÃÖ½ÂÂù
|
Vibration
Suppression of Rotating Composite Thin-walled Beam with
Piezoelectric Materials
|
¹Ú»ç
|
2004.8
|
±èÅ¿ì
|
Optimal Distribution
of Layer Damping for Transient Vibration Suppression
of Flexible Plates
|
¼®»ç
|
2004.2
|
Á¤Áø¿µ
|
Vibration Control of Stiffened Laminated Composite Plates with
Integrated Piezoelectrics |
¹Ú»ç |
2003.8 |
¹Ú½ÃÇü |
A
Posteriori Error Estimation and Adaptive Technique Based
on Variation of Maping Function |
¼®»ç |
2003.2 |
±â¿µÁß |
Vibration Chracteristics of Initially Twisted Rotating
Shell-type Blade
in Thermal Environment
|
¼®»ç |
2003.2 |
±èÈñ¿ø |
Influence of Piezoelectric Active Damper on The Dynamic
Stability of Structure
under A Thrust
|
¼®»ç |
2003.2 |
Á¤»ó¿ì |
Dynamic Stability of Liquid-Filled Cylindrical Shell under
Constant and Pulsating Follower Force |
¼®»ç |
2002.2 |
³ëÁøÈ£ |
Monitoring and Shape Control in Hybrid Smart Plate
under Low Velocity Impact |
¼®»ç |
2002.2 |
°í°æÀº |
Thermally Induced Vibration of Spinning Beam
Structures |
¼®»ç |
2001.2 |
³ª°æ¼ö |
Deployment of a
Multi-Link Flexible Beam Strcuture |
¼®»ç |
2001.2 |
±è¼º¼ö |
Breathing CrackÀÌ Àִ ȸÀüÇÏ´Â º¹ÇÕÀç·á ¿ÜÆȺ¸ÀÇ µ¿ÀûƯ¼º¿¡
°üÇÑ ¿¬±¸ |
¼®»ç |
2001.2 |
À±½ÂÁØ |
Effects of a Concentrated Mass on the
Spinning Free-Free Beam Subjected to a Thrust |
¼®»ç |
2000.2 |
ÀåÁ¤ÈÆ |
¿º¯ÇüÀ» °í·ÁÇÑ À¯¿¬ÇÑ ¿ìÁÖ±¸Á¶¹°ÀÇ Áøµ¿Çؼ® |
¼®»ç |
2000.2 |
±è»ó¿ø |
Àü°³µÇ´Â À¯¿¬ºÎÂø¹°À» °¡Áø ¿îµ¿Ã¼ÀÇ ¿îµ¿ Ư¼º º¯È ¿¬±¸ |
¼®»ç |
2000.2 |
³ëÈñ¿ |
ź¼ºÁöÁöºÎ¸¦ °¡Áø ȸÀüÇÏ´Â ºí·¹À̵åÀÇ Áøµ¿Çؼ® |
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1999.2 |
È«Á¦¹Î |
Àú¼Ó Ãæ°ÝÇÏÀÇ º¹ÇÕÀç·á ½©ÀÇ Ãæ°Ý °ËÃâ¿¡ °üÇÑ ¿¬±¸ |
¼®»ç |
1999.2 |
¹ÚÀçÈï |
ȸÀü ¿îµ¿À» ÇÏ´Â ³¡´Ü Áú·®À» °®´Â
°î¼±Çü»ó º¸ÀÇ µ¿Àû Çؼ® |
¼®»ç |
1999.2 |
±èÅ¿ì |
Á¡Åº¼ºÀ» °í·ÁÇÑ ³¡´Ü ÇÏÁßÀ» ¹Þ´Â º¹ÇÕÀç·á ¿ÜÆȺ¸ÀÇ ¾ÈÁ¤¼º Çؼ®
|
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1999.2 |
±è°æÈÆ |
Á¾µ¿·ÂÀ» ¹Þ´Â ¾ç´Ü ÀÚÀ¯ º¸ÀÇ µ¿Àû ¾ÈÁ¤¼º¿¡ Å©·¢ÀÌ ¹ÌÄ¡´Â ¿µÇâ¿¡ °üÇÑ
¿¬±¸ |
¼®»ç |
1998.2 |
¹Ú½ÃÇü |
ºÒ±ÔÄ¢ÇÑ ¿ÜºÎ±³¶õÀÌ ÁÖ±âÀû °¡ÁøÀ» ¹Þ´Â ºñ¼±Çü°èÀÇ µ¿Àû Ư¼º¿¡ ¹ÌÄ¡´Â
¿µÇâ |
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1998.2 |
³ªÇüÁø |
ºñ¼±Çü ÆÇÀÌ·ÐÀ» ÀÌ¿ëÇÑ È¸ÀüÇÏ´Â º¹ÇÕ Àç·á ÀûÃþÆÇÀÇ
Áøµ¿Çؼ® |
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1998.2 |
±èÇö¼ø |
Á¾µ¿·ÂÀ» ¹Þ´Â ¿øÅëÇü ½©ÀÇ µ¿Àû ¾ÈÁ¤¼º¿¡ °üÇÑ Çؼ® |
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1997.8 |
½Éµ¿Áø |
Àú¼Ó Ãæ°Ý½Ã °íÂ÷ ÆÇÀÌ·ÐÀ» ÀÌ¿ëÇÑ º¹ÇÕÀç·á ÀûÃþÆÇÀÇ µ¿Àû Ư¼º¿¡ °üÇÑ
Çؼ® |
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1997.2 |
Ãß¿¬¼± |
¸Æµ¿ Á¾µ¿·ÂÀÌ ÀÛ¿ëÇÏ´Â »ç´Ü ÀÚÀ¯°æ°è ÆÇÀÇ µ¿Àû ¾ÈÁ¤¼º¿¡ °üÇÑ
¿¬±¸ |
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1997.2 |
ÀÌ¿øö |
Á¾µ¿·ÂÀ» ¹ÞÀ¸¸ç ÀÚüÃà ÁÖÀ§·Î ȸÀüÇÏ´Â ¾ç´Ü ÀÚÀ¯º¸ÀÇ ¾ÈÁ¤¼º¿¡ °üÇÑ
¿¬±¸ |
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1996.2 |
Á¤Ãá»ó |
Áß·ÂÀÇ È¿°ú¸¦ °í·ÁÇÑ º¹ÇÕ Àç·á ÀûÃþº¸ÀÇ ºñ¼±Çü Áøµ¿
Çؼ® |
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1996.2 |
ÀÌ»ó¿í |
º¹ÇÕÀç·á ÀûÃþÆÇÀÇ ºñ¼±Çü ÀÚÀ¯ Áøµ¿Çؼ® |
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1996.2 |
¹ÚÁ¾Çö |
Áß°£´Ü¿¡ Á¾µ¿·ÂÀÌ ÀÛ¿ëÇÏ´Â ¿ÏÀü ÀÚÀ¯°æ°è ÆÇÀÇ µ¿Àû ¾ÈÁ¤¼º¿¡ °üÇÑ
¿¬±¸ |
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1995.2 |
±èÇö¼ö |
Á¾µ¿·ÂÀÌ ÀÛ¿ëÇÏ´Â º¹ÇÕÀç·á ÆòÆÇÀÇ µ¿Àû ¾ÈÁ¤¼º¿¡ °üÇÑ
Çؼ® |
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1995.2 |
³²Å¿ì |
Áß·ÂÀÇ È¿°ú¸¦ °í·ÁÇÑ º¹ÇÕÀç·á ÀûÃþº¸ÀÇ Áøµ¿ Çؼ® |
¼®»ç |
1994.2 |
°¿Õ±¸ |
±Õ¿ÀÌ ÀÖ´Â ÆòÆÇÀÇ ÀÀ·Â Çؼ® |