°í¼ÓÃßÁø ¹× ¿¬¼Ò½ÇÇè½Ç

+ ÇÑÁÙ °øÁö : ·Î±×ÀÎ ÇÏ¼Å¾ß °­ÀÇ °ü·Ã °Ô½ÃÆÇÀÇ ±ÛÀ» È®ÀÎÇÒ ¼ö ÀÖ½À´Ï´Ù.

sub menu
 

# Members

 
 

 ±³¼ö´Ô (Professor)

 

 

 Á¹¾÷»ý (Alumni)

 

 

 ½ÇÇè½Ç¿ø (Students)

 

gadget

[ HPCL ¿¬±¸ ³»¿ë ]

ÁøÇà ¿¬±¸ °úÁ¦

Á¾·á ¿¬±¸ °úÁ¦


½ÇÇè½Ç º¸À¯ Àåºñ

 

[ 2021-2 °­ÀÇ °Ô½ÃÆÇ]

[27148-00] ºñÇàÃßÁø½ÇÇè

[24087-00] ¿¡³ÊÁö¿Í¿­Àü´Þ

*·Î±×ÀÎ ÈÄ ÀÌ¿ëÇϼ¼¿ä.

[ ½ÇÇè½Ç ¾È³» ]

´ëÀü±¤¿ª½Ã À¯¼º±¸ ´ëÇзΠ99
Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú
(°ø´ë 3È£°ü 233È£)
'°í¼ÓÃßÁø ¹× ¿¬¼Ò ½ÇÇè½Ç'

Phone / 042 - 821 - 7771

FAX / 042 - 825 - 9225


ã¾Æ¿À½Ã´Â ±æ

 

 

 
 

¹Ú»ç (Doctor of Philosohpy : Ph.D.)

1

À̵¿ÈÆ »ï¼ºÅ×Å©À©(ÁÖ) -> SKÀ̳뺣À̼Ç(ÁÖ) -> µÎ»êÁß°ø¾÷(ÁÖ) -> µÎ»ê¿¡³Êºô¸®Æ¼(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¹Ú»ç('10.06)
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('99.02)
 

Ph.D. Dissertation

ºÐ¹«°¡½ÃÈ­¿Í À§»óÂ÷ µµÇ÷¯ ÃøÁ¤À» ÅëÇÑ °¡½ºÅͺó ȸÀüÇü ¿¬·áºÐ»ç±âÀÇ ºÐ¹« ¹× ¹Ì¸³È­ Ư¼º ¿¬±¸

 

Study on the Spray and Atomization Characteristics of the Rotary Atomizer for Gas Turbines using Spray Visualization and Phase Doppler Anemometry

Master Thesis

APV(Adaptive Phase/Doppler Velocimetry)¸¦ ÀÌ¿ëÇÑ ¸ðµ¨¿¬¼Ò±â³»ÀÇ ºÐ¹«Æ¯¼º¿¬±¸

 

A Study of Spray Characteristics in a Model Combustor using APV(Adaptive Phase Doppler Velocimetry)

 


2

°­¼±ÀÏ Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø(KARI) -> ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¹Ú»ç('12.02)
- ÀÎÇÏ´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('95)

 

Ph.D. Dissertation

¹° ºÐ»ç°¡ ·ÎÄÏ ¿¬¼ÒÈÄ·ù À¯µ¿Àå¿¡ ¹ÌÄ¡´Â ¿µÇâ¿¡ °üÇÑ ¿¬±¸

 

Numerical Study of the effects of the water spray on the Rocket Exhaust Plume

 


3

ÀÌÁß¿± Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø(KARI)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¹Ú»ç('14.02)

 

Ph.D. Dissertation

°³¹æ»çÀÌŬ ¾×ü·ÎÄÏ¿£Áø¿¡¼­ ¼ÓµµÁ¶Àý±â¹ýÀ» ÀÌ¿ëÇÑ Á¶Àý¹ëºêÀÇ Æ¯¼º¿¬±¸

 

Study on Characteristics of the Control Valve using the Speed Control Method for Open Cycle Liquid Rocket Engines

 


4

¹ÚÀÀ½Ä Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø(KARI)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¹Ú»ç('15.08)

 

Ph.D. Dissertation

Åë°èÀû ¹æ¹ýÀ» »ç¿ëÇÑ À§¼º ÀÜ¿©ÃßÁøÁ¦·® ÃßÁ¤±â¹ý ¿¬±¸

 

Study of Satellite Residual Propellant Estimation using Statistical Method

 


5

¼­ÈñÁØ Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø(KARI)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¹Ú»ç('16.08)
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('00.02)
 

Ph.D. Dissertation

±ØÀú¿Â ºí·Î¿ö ½Ã½ºÅÛ ¼º´É¿¹Ãø ¹× °ËÁõ¿¡ °üÇÑ ¿¬±¸

 

Study on Performance Prediction and Verification of a Cryogenic Blower System

Master Thesis

¿¢½Ã¸Ó ·¹ÀÌÀú¸¦ ÀÌ¿ëÇÑ ¿¡¸ÖÁ¯ ¿¬·áÀÇ ºÐ¹«Æ¯¼º ¿¬±¸

 

An Experimental study of the Atomization Characteristics using Excimer Laser in a Diesel Engine with Emulsion Fuels

 


6

¿ÀÈ­¿µ Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø(KARI)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¹Ú»ç
('17.08)
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç
('07.02)
 

Ph.D. Dissertation

·ÎÄÏ ¿£Áø ¿¬¼Ò ÈÄ·ù·Î ÀÎÇÑ ¹ß»ç´ë Áö»ó¼³ºñ ¿µÇ⼺ ºÐ¼®¿¡ °üÇÑ ¿¬±¸

 

Study on the Influence Analysis of Launch Complex Ground Equipment by Engine Exhaust Gas of Launch Vehicle

Master Thesis

¿¬·á ÀüÁö¿¡ÀÇ Àû¿ëÀ» À§ÇÑ ¼ÒÇü½ºÀ§½º·Ñ ¿¬¼Ò±â ¼º´É¿¡ ´ëÇÑ Å©±â¿Í Çü»ó È¿°ú

 

Effect of geometry and scale on the performance of small-scale heat-recirculating swiss-roll combustor for fuel cel applications

 


7

±è»óÈ£ Çѱ¹Ç×°ø¿ìÁÖ»ê¾÷(KAI)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¹Ú»ç('19.02)
- ÀÎÇÏ´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç

 

Ph.D. Dissertation

ÀΰøÀ§¼º žÀçÇ°¿¡ ¿­Áø°ø½ÃÇè °¡¼ÓÈ­ ¾Ë°í¸®Áò ¿¬±¸

 

Research for Optimized Algorithm for Thermal Vacuum Test Acceleration of Satellite Components

 


8

ÀÌÀçû (ÁÖ)½êÆ®·º¾ÆÀÌ

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¹Ú»ç('20.08)
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('15.02)

 
- Fluent Solver Basic ±³À° (2013. 03)
- Prop. Servo & Troubleshooting Course (2014.04)
- AMESim Basic Training (2014.09)
- AMESim Advanced Training(Hydraulic Advanced) (2014.09)

- À¯µµÅºÃßÁø±â°ü ±â¼ú[½ÉÈ­] Part 1 (2015.09)
Àü¹®±â¼ú±³À° źµµÀ¯µµ¹«±â(Àü¹®) ±³À° (2017.03)
-
Àü¹®±â¼ú±³À° À¯µµÅº ÃßÁø±â°ü±â¼ú-II ±³À° (2017.09)
 

Ph.D. Dissertation

ÃÊ°í¼Ó ºñÇàüÀÇ ¼±µÎºÎ¿¡¼­ ¿ªºÐ»ç Á¦Æ®¿¡ ÀÇÇÑ À¯µ¿ Ư¼º°ú Ç×·Â °¨¼Ò ¿¬±¸

 

Study of Flow Characteristics and Drag Reduction by Counterflow Jets at the Nose Cone of a High-speed Vehicle

Master Thesis

è¹ö¸¦ °øÀ¯ÇÏ´Â 2Ãà ÇÉƲ Ã߷±⠽ýºÅÛ¿¡ °üÇÑ ¼öÄ¡Àû ¿¬±¸

 

A Numerical Study on Two-Axis Pintle Thrusters with a Chamber

 


 
 

¼®»ç (Master)

1

ÁغñÁßÀÔ´Ï´Ù

ÀÌÀçÈ£ Çѱ¹ÇÏ´ÏÀ£

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('98.02)

 

Master Thesis

4-¹ëºê SI ¿£Áø¿¡¼­ÀÇ È­¿°°¡½ÃÈ­

 

Flame Visualization in 4-Valve SI Engine

 

2

ÁغñÁßÀÔ´Ï´Ù

±èÁ¤¹Î »ï¼ºÀü±â(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('98.02)

 

Master Thesis

Á¤Àû¿¬¼Ò½Ç¿¡¼­ ¿¹È¥ÇÕ±âÀÇ ¿¬¼Ò¼Óµµ ÃøÁ¤

 

Measurement of buring velocities of premixed mixtures in a constant-volume combustion chamber

 


3

À̵¿ÈÆ »ï¼ºÅ×Å©À©(ÁÖ) -> SKÀ̳뺣À̼Ç(ÁÖ) -> µÎ»êÁß°ø¾÷(ÁÖ) -> µÎ»ê¿¡³Êºô¸®Æ¼(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¹Ú»ç('10.06)
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('99.02)
 

Ph.D. Dissertation

ºÐ¹«°¡½ÃÈ­¿Í À§»óÂ÷ µµÇ÷¯ ÃøÁ¤À» ÅëÇÑ °¡½ºÅͺó ȸÀüÇü ¿¬·áºÐ»ç±âÀÇ ºÐ¹« ¹× ¹Ì¸³È­ Ư¼º ¿¬±¸

 

Study on the Spray and Atomization Characteristics of the Rotary Atomizer for Gas Turbines using Spray Visualization and Phase Doppler Anemometry

Master Thesis

APV(Adaptive Phase/Doppler Velocimetry)¸¦ ÀÌ¿ëÇÑ ¸ðµ¨¿¬¼Ò±â³»ÀÇ ºÐ¹«Æ¯¼º¿¬±¸

 

A Study of Spray Characteristics in a Model Combustor using APV(Adaptive Phase Doppler Velocimetry)

 


4

¹Ú½ÂÈÆ (ÁÖ)»ï¼ºÅ»·¹½º -> À̽ºÅ¸Ç×°ø(ÁÖ) -> Ç×°ø¾ÈÀü±â¼ú¿ø(KIAST) -> À̽ºÅ¸Ç×°ø(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('99.02)

 

Master Thesis

¸ðµ¨ ¿¬¼Ò±â³»ÀÇ ¿ÂµµÀå ÃøÁ¤ ¹× È­¿° °¡½ÃÈ­¸¦ ÅëÇÑ ¹®¹«¿¬¼ÒƯ¼º ¿¬±¸

 

Study of spray combustion characteristics in a model combustor through temperature measurements and flame visualization

 


5

¼­ÈñÁØ Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø(KARI)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¹Ú»ç('16.08)
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('00.02)
 

Ph.D. Dissertation

±ØÀú¿Â ºí·Î¿ö ½Ã½ºÅÛ ¼º´É¿¹Ãø ¹× °ËÁõ¿¡ °üÇÑ ¿¬±¸

 

Study on Performance Prediction and Verification of a Cryogenic Blower System

Master Thesis

¿¢½Ã¸Ó ·¹ÀÌÀú¸¦ ÀÌ¿ëÇÑ ¿¡¸ÖÁ¯ ¿¬·áÀÇ ºÐ¹«Æ¯¼º ¿¬±¸

 

An Experimental study of the Atomization Characteristics using Excimer Laser in a Diesel Engine with Emulsion Fuels

 


6

¼­Á¤¿ø (ÁÖ)ÇѾó½Ã½ºÅÛ

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('02.02)

 

Master Thesis

Ãà¿­½Ä »ê¼ÒºÎÈ­¿¬¼Ò±âÀÇ Áú¼Ò »êÈ­¹°(NOx) Àú°¨ ¹æ¹ý¿¡ °üÇÑ ½ÇÇèÀû ¿¬±¸

 

An Experimental Study of Low NOx Comnustion for Regenerative Oxygen Enriched Combustor

 


7

±èÁ¤¿ë »ï¼º ¿£Áö´Ï¾î¸µ

- ¹Ì³×¼ÒŸ ÁÖ¸³´ëÇÐ ¹Ú»ç
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('02.02)

 

Master Thesis

½ºÅ©·¥ Á¦Æ® Àû¿ëÀ» À§ÇÑ Ãß·Â ÃøÁ¤ ¹æ¹ý ¿¬±¸ ¹× 2Â÷¿ø ÃÊÀ½¼Ó dzµ¿ÀÇ ¼³°è

 

A Study of Thrust Determination Method and Design of 2-D Supersonic Wind Tunnel for Scramjet Applications

 


8

Á¤À¯¼® Çѱ¹Àü·Â±â¼ú

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('03.02)

 

Master Thesis

Ãà¿­½Ä »ê¼ÒºÎÈ­¿¬¼Ò½Ã½ºÅÛ ¼º´ÉÇâ»óÀ» À§ÇÑ ¼¼¶ó¹Í Çã´ÏÄÄ Ã࿭üÀÇ ½ÇÇèÀû ¿¬±¸

 

An Experimental Study of Ceramic Honeycomb Regenerator of Oxygen Enriched Regenerative Combustion System

 


9

ÀÌÇý¿µ Çѱ¹±â°è¿¬±¸¿ø(KIMM)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('03.02)

 

Master Thesis

¿¡³ÊÁöÀý¾à¿ë ¼¼Â÷Á¦Æ® ³ëÁñÀÇ À¯µ¿ Ư¼º¿¡ ´ëÇÑ ¿¬±¸

 

A Study of Fluidic Characteristics of Precessing Jet Nozzle for Energy saving application

 


10

¹Ú½ÂÀç Çö´ë¿ìÁÖÇ×°ø -> (ÁÖ)ÇÑÈ­ -> (ÁÖ)Çö´ëÆÄ¿öÅØ -> Çö´ëÆ®·»½Ã½º(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('03.02)

 

Master Thesis

¾Æ¼¼Åæ PLIFÀ» ÀÌ¿ëÇÑ °ø¿¬ºñ ÃøÁ¤ ±â¹ýÀÇ ¿¬±¸

 

An Experimental Study of Measurement Technique of Air Fuel Ratio using Aceton PLIF

 


11

±èÀÎÅ (ÁÖ)ÇÑÈ­ -> (ÁÖ)µ¥ÀÓ

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('03.08)

 

Master Thesis

¼ÒÇü ¾×ü ÃßÁø±â°ü ¿¬¼Ò ½ÃÇèÀ» À§ÇÑ Ãß·Â ÃøÁ¤ ÀåÄ¡ÀÇ ¼º´É Ư¼º ¿¬±¸

 

A Study on the Performance Characteristics of Thrust Measurement System for Hot-Firing Test of Small Liquid Propulsion Engines

 


12

±èÇü¹Î (ÁÖ)COAVIS

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('04.02)

 

Master Thesis

¾Ð·ÂÃøÁ¤ °á°ú¸¦ ÀÌ¿ëÇÑ °í¼ÓÃßÁø±â°üÀÇ Ãß·ÂÃøÁ¤¿¡ °üÇÑ ¿¬±¸

 

A Study of Thrust Measurement from Pressure Measurement for High Speed Propulsion System

 


13

¹®¼ºÈ¯ (ÁÖ)COAVIS -> Vitesco TECHNOLOGIES 

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('05.02)

 

Master Thesis

¸¶ÀÌÅ©·Î ÃßÁøÀåÄ¡¿¡ ´ëÇÑ ±âÃÊ ½ÇÇè

 

Preliminary Experiment for Micro Propulsion Device

 


14

¿ÀÈ­¿µ Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø(KARI)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¹Ú»ç
('17.08)
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç
('07.02)
 

Ph.D. Dissertation

·ÎÄÏ ¿£Áø ¿¬¼Ò ÈÄ·ù·Î ÀÎÇÑ ¹ß»ç´ë Áö»ó¼³ºñ ¿µÇ⼺ ºÐ¼®¿¡ °üÇÑ ¿¬±¸

 

Study on the Influence Analysis of Launch Complex Ground Equipment by Engine Exhaust Gas of Launch Vehicle

Master Thesis

¿¬·á ÀüÁö¿¡ÀÇ Àû¿ëÀ» À§ÇÑ ¼ÒÇü½ºÀ§½º·Ñ ¿¬¼Ò±â ¼º´É¿¡ ´ëÇÑ Å©±â¿Í Çü»ó È¿°ú

 

Effect of geometry and scale on the performance of small-scale heat-recirculating swiss-roll combustor for fuel cel applications

 


15

Á¤¼ºÃ¶ µÎ»êÁß°ø¾÷(ÁÖ) -> µÎ»ê¿¡³Êºô¸®Æ¼(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('08.02)

 

Master Thesis

¸¶ÀÌÅ©·Î ÃßÁøÀåÄ¡¿¡ Àû¿ëÀ» À§ÇÑ Áø°ø ȯ°æ¿¡¼­ ¿­Àû¹ß»êÀåÄ¡ÀÇ È¿À² ºÐ¼®

 

Efficiency analysis of thermal transpiration for application to micro-propulsion system under vacuum condition

 


16

±è¿¬È£ (ÁÖ)½êÆ®·º¾ÆÀÌ

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('08.02)

 

Master Thesis

¿¬·áÀüÁö¿¡ÀÇ Àû¿ëÀ» À§ÇÑ ½ºÀ§½º·Ñ ¿¬¼Ò±âÀÇ Å©±â¿Í ¿¬·á¿¡ µû¸¥ Ư¼º ¿¬±¸

 

Study of scale and fuel-type on the performance of micro-scale heat-recirculating Swiss-roll combustor for fuel cell applications

 


17

À̹ÎÀç STX Áß°ø¾÷(ÁÖ) -> ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('08.08)

 

Master Thesis

Áø°ø »óÅ ¹× ÆØâºñ º¯È­¿¡ µû¸¥ ¸¶ÀÌÅ©·Î ³ëÁñÀÇ Ã߷ Ư¼º ¿¬±¸

 

Study of thrust characteristic for micro nozzle with vacuum condition and expansion ratio variation

 


18

½Å°­Ã¢ »ï¼ºÅ×Å©À©(ÁÖ) -> (ÁÖ)»ï¼ºÀüÀÚ

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('09.02)

 

Master Thesis

¿¬·áÀüÁö¿¡ÀÇ Àû¿ëÀ» À§ÇÑ ¼ÒÇü Çöó½ºÆ½ ¿¬¼Ò±âÀÇ Å©±â¿Í Çü»ó¿¡ µû¸¥ Ư¼º¿¬±¸

 

Study of Scale and geometry on the Performance of Small-scale Plastic Swiss-roll combustor for Fuel cell Applications

 


19

±èÇýȯ (ÁÖ)ÇÑÈ­ -> ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('09.08)

 

Master Thesis

¸¶ÀÌÅ©·Î ÃßÁøÀåÄ¡¿¡ÀÇ Àû¿ëÀ» À§ÇÑ ´©¼¾ ÆßÇÁÀÇ ±âÃʽÇÇè

 

Basic Experiment of Knudsen Pump for Application to Micro-propulsion System

 


20

ÀÌÁ¾·ü (ÁÖ)ÇÑÈ­ -> ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('10.02)

 

Master Thesis

À§¼ºÅ¾ÀçÄ«¸Þ¶óÀÇ ¿­Áø°ø ½ÃÇè ¿ÂµµÁ¶°Ç Çؼ®

 

Analysis of Thermal Condition for Thermal Vacuum Tests of Satellite's Optical Camera

 


21

ÀÌ¿ë¿ì (ÁÖ)ÇÑÈ­ -> ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('10.08)

 

Master Thesis

DACS(Divert and Attitude Control System)¿¡ Àû¿ë °¡´ÉÇÑ ÇÉƲ ³ëÁñÀÇ ¼öÄ¡Çؼ®Àû ¿¬±¸

 

Computational Analysis of Pintle Nozzle for DACS(Divert and Attitude Control System)

 


22

À±µ¿ÀÍ (ÁÖ)ÇÑÈ­ -> ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('11.02)

 

Master Thesis

Áø°ø ȯ°æ¿¡¼­ ¿­Àû¹ß»ê¿ø¸®¸¦ ÀÌ¿ëÇÑ ´©¼¾ÆßÇÁ ¸âºê·¹ÀΠƯ¼º¿¡ °üÇÑ ¿¬±¸

 

Study of Knudsen Pump Membrane Characteristic using Thermal Transpiration under Vacuum Condition

 


23

°­¿Ï±Ô LIG Nex1(ÁÖ) -> °³ÀÎ »ç¾÷(´ëÇ¥)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('11.02)

 

Master Thesis

ÇÏÀ̺긮µå ·ÎÄÏÀÇ ÃßÁøÁ¦ Á¾·ù¿¡ µû¸¥ ¿¬¼ÒƯ¼º ¹× Ãß·ÂÁ¦¾î ½ÇÇè

 

Experiment on the combustion characteristics and thrust control according to the propellant type of hybrid rockets

 


24

±è¹ÎÀç LIG Nex1(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('12.02)

 

Master Thesis

Àú±Ëµµ À§¼º ±¤ÇОÀçüÀÇ ¿­Áø°ø½ÃÇè °á°ú¸¦ È°¿ëÇÑ °ËÁõµÈ ¿­Çؼ® ¸ðµ¨ °³¹ß ¿¬±¸

 

Development of Thermal Analysis Model using Results of LEO Satellite Optical Payload's Thermal Vacuum Test

 


25

ÃÖÀ缺 LIG Nex1(ÁÖ) -> ±¹¹æ±â¼úÇ°Áú¿ø(DTAQ) -> ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('12.02)

 

Master Thesis

°¡º¯Çü ³ëÁñÀ» ÀÌ¿ëÇÑ Ãß·ÂÁ¦¾î ±â¹ýÀÇ ½ÇÇèÀû ¿¬±¸

 

An Experimental Study of Thrust Control for Modulatable Thruster Applications

 


26

¿Õ½Â¿ø Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø(KARI)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('12.08)

- Sinda/Fluint ±âº» ±³À° (2010. 01)
- LabView 2010 ±âº» ±³À° (2010. 01)
- Fluent ±âº» ±³À° (2010. 05, 2011. 09)
- ·ÎÄÏ ÃßÁø°³¹ß ½Ç¹« ¹× È°¿ë ´Ü±â°­Á (2010. 08)
- Fluent Turbulence °úÁ¤ (2011. 01)
- Fluent Heat Transfer °úÁ¤ (2011. 02)
- Ansys Combustion ±³À° (2011. 05)

Master Thesis

ÇÉƲ±¸µ¿ÀåÄ¡Çü °íüÃ߷±âÀÇ ¼º´ÉÇâ»óÀ» À§ÇÑ Çü»ó¼³°è ¿¬±¸

 

The Shape Design Study for Efficiency Improvement of Modulatable Thruster

 


27

À̼±°æ (ÁÖ)ºñÃ÷·ÎÅ×Å© -> ¾Á¸µÅ©(ÁÖ) -> °³Àλç¾÷(´ëÇ¥)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('12.08)

- LabView 2010 ±âº» ±³À° (2010. 01)
- Fluent ±âº» ±³À° (2010. 05, 2011. 09)
- ·ÎÄÏ ÃßÁø°³¹ß ½Ç¹« ¹× È°¿ë ´Ü±â°­Á (2010. 08)
- Fluent Turbulence °úÁ¤ (2011. 01)
- Fluent Heat Transfer °úÁ¤ (2011. 02)
- Ansys Combustion ±³À° (2011. 05)
- ¿¬±¸³ëÆ® ÀÛ¼º °úÁ¤ ±³À°(2012. 02)
 

Master Thesis

ÇÉƲÀÌ ±¸µ¿ÇÏ´Â ³ëÁñÀÇ ¼öÄ¡Çؼ®Àû °ËÁõ ¿¬±¸

 

Computational Analysis of Pintle Driven Nozzle

 


28

±èµ¿¿¬ ÆÛ½ºÅØ(ÁÖ) -> (ÁÖ)À¯¾ÆÀÌƼ -> (ÁÖ)Å°ÇÁÄÚÀüÀÚÇ×°ø

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('13.08)

- ¿¬±¸³ëÆ® ÀÛ¼º °úÁ¤ ±³À°(2012. 02)
- Fluent Solver Basic ±³À° (2012. 03)
- Fluent Dynamic Mesh ±³À°(2012.08)
- Fluent UDF ±³À°(2012.09)
 

Master Thesis

³ëÁñ¸ñ ³»·¿ÜºÎÇü ÇÉƲ Ã߷±âÀÇ CFD ¸ð»ç¸¦ ÀÌ¿ëÇÑ ¿¬±¸

 

CFD Simulation of a Nozzle Throat for Inside- and Outside-Type Pintle Thrusters

 


29

±è¼º¼ö (ÁÖ)ÇÑÈ­ -> ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('13.08)

- Fluent ±âº» ±³À° (2011. 09)
- ¿¬±¸³ëÆ® ÀÛ¼º °úÁ¤ ±³À°(2012. 02)

- AMESim Basic Training(2012. 02)
- LabView Core 1 Course(2012.08)
 

Master Thesis

ÇÉƲ Ã߷±âÀÇ ¾Ð·ÂÁ¦¾î ±â¹ý¿¡ °üÇÑ ½ÇÇèÀû ¿¬±¸

 

An Experimental Study of Pressure Control Method for Modulatable Thruster Applications

 


30

ÀÌÀçû (ÁÖ)½êÆ®·º¾ÆÀÌ

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¹Ú»ç('20.08)
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('15.02)

 
- Fluent Solver Basic ±³À° (2013. 03)
- Prop. Servo & Troubleshooting Course (2014.04)
- AMESim Basic Training (2014.09)
- AMESim Advanced Training(Hydraulic Advanced) (2014.09)

- À¯µµÅºÃßÁø±â°ü ±â¼ú[½ÉÈ­] Part 1 (2015.09)
Àü¹®±â¼ú±³À° źµµÀ¯µµ¹«±â(Àü¹®) ±³À° (2017.03)
-
Àü¹®±â¼ú±³À° À¯µµÅº ÃßÁø±â°ü±â¼ú-II ±³À° (2017.09)
 

Ph.D. Dissertation

ÃÊ°í¼Ó ºñÇàüÀÇ ¼±µÎºÎ¿¡¼­ ¿ªºÐ»ç Á¦Æ®¿¡ ÀÇÇÑ À¯µ¿ Ư¼º°ú Ç×·Â °¨¼Ò ¿¬±¸

 

Study of Flow Characteristics and Drag Reduction by Counterflow Jets at the Nose Cone of a High-speed Vehicle

Master Thesis

è¹ö¸¦ °øÀ¯ÇÏ´Â 2Ãà ÇÉƲ Ã߷±⠽ýºÅÛ¿¡ °üÇÑ ¼öÄ¡Àû ¿¬±¸

 

A Numerical Study on Two-Axis Pintle Thrusters with a Chamber

 


31

ȲÈñ¼º ±¹¹æ°úÇבּ¸¼Ò(ADD) -> (ÁÖ)½êÆ®·º¾ÆÀÌ -> ±¹¹æ°úÇבּ¸¼Ò(ADD)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('16.02)

- LabView Core 1 Course(2012.08)

- Fluent Solver Basic ±³À° (2013.03)

 

Master Thesis

³»ºÎÇü ÇÉƲ Ã߷±âÀÇ ºñÁ¤»ó»óÅ Ư¼º ¹× ¿ÜºÎÇü ÇÉƲ Ã߷±âÀÇ À¯µ¿Æ¯¼º ¿¬±¸

 

Unsteady State Characteristics of an Inside Pintle Thruster and Flow Characteristics of an Outside Pintle Thruster

 


32

³ë¼ºÇö (ÁÖ)ÇÑÈ­ -> ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('16.02)

- ANSYS FLUENT ÀÔ¹®°úÁ¤ (2013.08)
 

Master Thesis

ÇÉƲ Ã߷±âÀÇ ³ëÁñ Çü»óº° ¼º´É ¹× À¯µ¿Æ¯¼º¿¡ °üÇÑ ¿¬±¸

 

Performance and Flow Characteristics of a Pintle Thruster According to Nozzle Contours

 


33

±èÁöÈ« (ÁÖ)ÇÑÈ­ -> ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('16.08)

- ANSYS FLUENT ÀÔ¹®°úÁ¤ (2013.08)
 

Master Thesis

ÃÊÀ½¼Ó dzµ¿ ¼º´É °ËÁõ ¹× ÀÌÂ÷ À¯µ¿ ºÐ»ç¿¡ µû¸¥ À¯µ¿ º¯È­ ¿¬±¸

 

Performance Test of Supersonic Wind Tunnel and Effects of Secondary Flow Injection on the Supersonic Flow

 


34

±èÁ¤ÈÆ ±¹¹æ°úÇבּ¸¼Ò(ADD) -> (ÁÖ)ÇÑÈ­ -> ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('17.02)

 

Master Thesis

Çѱ¹Çü¹ß»çü¸¦ ±â¹ÝÀ¸·Î ÇÑ µà¾ó º§ ³ëÁñÀÇ ÃµÀÌ Æ¯¼º ¹× ¼º´É À̵æ

 

Transition Characteristics and Performance Gain of a Dual Bell Nozzle Based on the KSLV-II Launch Vehicle

 


35

°­½Â¿ø Çѱ¹±â°è¿¬±¸¿ø(KIMM) -> ±¹¹æ±â¼úÁøÈ↓±¸¼Ò(KRIT)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('18.02)

 

Master Thesis

Ç׷°¨¼Ò¸¦ À§ÇÑ ÇöóÁ ºÐ»çÀåÄ¡ ±âÃÊ ½ÇÇè ¿¬±¸

 

Fundamental Test of Plasma Counterflow Jets for Drag Reduction Applications

 


36

¹®Å¼® Çѱ¹°úÇбâ¼ú±âȹÆò°¡¿ø(KISTEP)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('18.02)

- ANSYS FLUENT ±âº» ±³À° (2016.07)
 

Master Thesis

Çѱ¹Çü¹ß»çü¸¦ ±â¹ÝÀ¸·Î ÇÑ °íµµº¸Á¤¿ë È®Àå-±¼Àý(E-D) ³ëÁñÀÇ ¼º´É Ư¼º ¹× ºñÃß·Â ÀÌµæ ¿¬±¸

 

Performance Characteristics and Specific Impulse Gain of an Expansion-Defection Nozzle for Altitude Compensation Nozzle based on the KSLV-II Launch Vehicle

 


37

¹Ú»óÇö ±¹¹æ±â¼úÁøÈ↓±¸¼Ò(KRIT)
 
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('18.02)

- ANSYS FLUENT ±âº» ±³À° (2016.07)
 

Master Thesis

°íµµº¸Á¤¿ë È®Àå-±¼Àý(E-D) ³ëÁñÀÇ ³ëÁñ ¾Ð·Âºñ¿¡ µû¸¥ Á¤»ó»óÅ À¯µ¿ Ư¼º ¿¬±¸

 

Steady State Flow Characteristics of an E-D(Expansion-Deflection) Nozzle for Altitude Compensation According to Nozzle Pressure Ratio

 


38

ÃÖÁ¾ÀÎ °ø¹«¿ø

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('18.02)

 - ANSYS FLUENT ÀÔ¹®ÀÚ ±³À° (2016.09)
 

Master Thesis

¿ªºÐ»ç °ø±â/ÇöóÁ Á¦Æ®¸¦ Àû¿ëÇÑ °í¼Ó ºñÇàüÀÇ À¯µ¿ ±¸Á¶ ¹× Ç×·Â °¨¼Ò¿¡ °üÇÑ ½ÇÇèÀû ¿¬±¸

 

An Experimental Study on the Flow Structure and Drag Reduction of a High Speed Vehicle using Counterflow Air/Plasma Jets

 


39

±èÇÑ¼Ö ±¹¹æ±â¼úÁøÈ↓±¸¼Ò(KRIT)

- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('19.02)

Àü¹®±â¼ú±³À° źµµÀ¯µµ¹«±â(Àü¹®) ±³À° (2017.03)
-
Àü¹®±â¼ú±³À° ´ë°øÀ¯µµ¹«±â(Àü¹®) ±³À° (2017.03)
-
ANSYS FLUENT ÀÔ¹®ÀÚ ±³À° (2017.07)
-
Àü¹®±â¼ú±³À° À¯µµÅº ÃßÁø±â°ü±â¼ú-II ±³À° (2017.09)
-
ANSYS FLUENT Heat Transfer ±³À° (2018.07)
-
ANSYS FLUENT Combustion ±³À° (2018.07)
 

Master Thesis

¸Þź°¡½º ¹°¼ºÄ¡¸¦ Àû¿ëÇÑ ³ëÁñ¸ñ ¿ÜºÎÇü ÇÉƲ ³ëÁñÀÇ Á¤»ó»óÅ À¯µ¿ Ư¼º ¿¬±¸

 

A Study on the Characteristics of Steady-State Flows of the External Pintle Nozzle with Methan Gas Properties

 


40

ÀÌÀ¯¼® ±¹¹æ°úÇבּ¸¼Ò(ADD)

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('20.02)

Àü¹®±â¼ú±³À° źµµÀ¯µµ¹«±â(Àü¹®) ±³À° (2017.03)
-
ANSYS FLUENT ÀÔ¹®ÀÚ ±³À° (2017.07)
-
Àü¹®±â¼ú±³À° źµµÀ¯µµ¹«±â(½ÉÈ­) ±³À° (2018.03)
-
Àü¹®±â¼ú±³À° À¯µµ¹«±â ±¸µ¿ÀåÄ¡ ±³À° (2018.03)
-
ANSYS FLUENT Heat Transfer ±³À° (2018.07)
 

Master Thesis

Free-jet ŸÀÔ ÃÊÀ½¼Ó dzµ¿ ±¸Ãà ¹× ¿ªºÐ»ç Á¦Æ® Ư¼º ºÐ¼® ½ÇÇè ¿¬±¸

 

Design and Construction of the Free-jet Type Supersonic Wind Tunnel and Experimental Study on the Characteristic Analysis for Counterflow Jets

 


41

À̱âȯ ±¹¹æ±â¼úÁøÈ↓±¸¼Ò(KRIT) -> ±¹¹æ°úÇבּ¸¼Ò(ADD)

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('20.02)

-
ANSYS FLUENT ÀÔ¹®ÀÚ ±³À° (2017.07)
-
ANSYS FLUENT Basic ±³À° (2018.07)
-
¿À½Ç·Î½ºÄÚÇÁ ½Ç½À ±³À° (2018.07)
-
CAE ±âÃÊ ±¸Á¶Çؼ® ±³À° (2019.03)
-
Àü¹®±â¼ú±³À° ´ë°øÀ¯µµ¹«±â(Àü¹®) ±³À° (2019.03)
-
¾×ü·ÎÄÏ ¿£Áø ¼³°è ´Ü±â°­Á (2019.06)
-
Àü¹®±â¼ú±³À° ±¹¹æ¼ÒÀç ±â¼ú(Àü¹®) ±³À° (2019.08)
-
Àü¹®±â¼ú±³À° °íüÃßÁø±â°ü I(Àü¹®) ±³À° (2019.09)
 

Master Thesis

Çѱ¹Çü¹ß»çü¸¦ ±â¹ÝÀ¸·Î ÇÑ È®Àå-±¼Àý(E-D) ·ÎÄÏ ³ëÁñÀÇ ¼³°è º¯¼ö Ư¼º ¿¬±¸

 

Parametric Study on the Design of an Expansion-Deflection(E-D) Rocket Nozzle Based on the KSLV-II Launch Vehicle

 


42

¹é°æ¹Ì ±¹¹æ±â¼úÁøÈ↓±¸¼Ò(KRIT) -> ±¹¹æ±â¼úÇ°Áú¿ø(DTAQ)

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('21.02)

- »ê¾÷Åë»óÀÚ¿øºÎ ¿¬±¸Áö¿øÀü¹®°¡ (2018.04)
 

Master Thesis

º¹ÇÕÃßÁø ½Ã½ºÅÛ Àû¿ëÀ» À§ÇÑ °¡½ºÅÍºó ¿£Áø ¸ðµâÀÇ µ¿Àû ¸ðµ¨¸µ

 

Dynamic Modeling of an Gas Turbine Engine Module for Integrated Propulsion Systems

 


43

±â¿ø±Ù ±¹¹æ±â¼úÁøÈ↓±¸¼Ò(KRIT)

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ ¼®»ç('21.02)

-
CAE ±âÃÊ ÀüÀÚ±âÀåÇؼ® ±³À° (2019.03)
- Àü¹®±â¼ú±³À° ´ë°øÀ¯µµ¹«±â(Àü¹®) ±³À° (2019.03)
-
Àü¹®±â¼ú±³À° ±º¿ë Àü¿ø/ÀüÁö ±â¼ú(Àü¹®) ±³À° (2019.04)
-
¾×ü·ÎÄÏ ¿£Áø ¼³°è ´Ü±â°­Á (2019.06)
-
Àü¹®±â¼ú±³À° °íüÃßÁø±â°ü I(Àü¹®) ±³À° (2019.09)
- AMESim Basic ±³À° (2020.07)

 

Master Thesis

Àü±âÆßÇÁ »çÀÌŬÀÇ ÃßÁøÁ¦ °ø±Þ ½Ã½ºÅÛ Â÷¾Ð ¿ä¼Ò ¸ð»ç ½ÇÇè ¿¬±¸

 

Experimental Study on Simulating Differential Pressure Components in the Propellant Supply System of an Electric Pump Cycle


44

±è°Ç¿µ ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú ¼®»ç('23.02)

- Labview ÄÚ¾î 2(Áß±Þ) ±³À° (2022.02)
- Labview PLC ¹× Åë½Å ±³À° (2022.10)

- AIAA °­ÁÂ(Advanced Space Propulsion) ±³À° (2023.01)

- ANSYS Fluent ÀÔ¹® ±³À° (2023.02)

- ANSYS Mechanical ÀÔ¹® ±³À° (2023.02)

- ANSYS Electromagnetics ÀÔ¹® ±³À° (2023.02)

 

Master Thesis

Experimental Study on Flow Control System of an Electric Pump-fed Cycle Space Propulsion System

 


45

ÀÌÁÖ¹Ì ±¹¹æ°úÇבּ¸¼Ò(ADD)

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú ¼®»ç('23.02)

- ANSYS Mechanical ±³À°(2021.08)
- AIAA °­ÁÂ(Design of Experiments) ±³À° (2023.01)

- ANSYS Fluent ÀÔ¹® ±³À° (2023.02)

- ANSYS Mechanical ÀÔ¹® ±³À° (2023.02)

 

Master Thesis

A Study on the Characteristics of Steady-State Flow of Expansion-Deflection(E-D) Nozzles with Reduced Lengths of Nozzle Extension

 


46

±èÁØ°â ÷´Ü¼ö¼Ûü¿¬±¸¼Ò -> ±¹¹æ°úÇבּ¸¼Ò(ADD)

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú ¼®»ç('23. 08)

- NX CAD basic ±³À° (2022.11)
- NX CAE Advanced Simulation ±³À° (2022.11)

- NX CAE Thermal & Flow Basic ±³À° (2022.12)

 

Master Thesis

Experimental Study on Performance Characteristics of Effective Emissivity for Space-borne Multi-Layer Insulation

 


47

À̹ÎÈ£ ¹Ì·¡¸ðºô¸®Æ¼½Ã½ºÅÛ¿¬±¸¼Ò -> ±¹¹æ°úÇבּ¸¼Ò(ADD)

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú ¼®»ç('24. 02)

- Battery & BMS ±³À° (2022.07)
 

Master Thesis

Study on Thermal Characteristic of Lithium-Ion Batteries in Response to Vacuum Pressure Variations

 

 


48

¿°°æÈÆ(ÆÄÆ® ŸÀÓ ¼®»ç) Æ丮Áö¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)


Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú ¼®»ç('24. 02)

 

Master Thesis

V-notchÇü ±ØÀú¿Â º¼ ¹ëºê¸¦ ÀÌ¿ëÇÑ ·ÎÄÏ¿£ÁøÀÇ Ãß·ÂÁ¦¾î ¿¬±¸

 

A Study on Integrated Cryogenic Control Valve with Injector

 


49

¼ÕÁßÈÆ ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú ¼®»ç('25.02)

- Labview ÄÚ¾î 2(Áß±Þ) ±³À° (2023.08)
 

Master Thesis

Àü±âÆßÇÁ »çÀÌŬ ¿£ÁøÀÇ ÅÊÅ© °¡¾Ð°ú P °ÔÀο¡ µû¸¥ ÃßÁøÁ¦ °ø±Þ ÀÀ´ä Ư¼º ¿¬±¸

 

A Study on Propellant Supply Response Characteristics of Electric Pump-fed Cycle Engines according to Tank Pressurization and P gain

 


50

ÀÌâÁ¾ ¹Ì·¡¸ðºô¸®Æ¼½Ã½ºÅÛ¿¬±¸¼Ò

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú ¼®»ç('25.02)

- Fluent multiphase(°í±Þ) ±³À° (2024.02)

- Fluent battery thermal management ±³À°(2024.04)
 

Master Thesis

Àç»ý³Ã°¢Çü ÇÉƲÀÇ ¿­À¯µ¿ Çؼ® ÀÎÇϿ콺 ÄÚµå °³¹ß ¹× ³Ã°¢ À¯·Î ¼ö·ù½ÃÇè

 

Development of an In-house Code for Thermal-Fluid Analysis of Regenerative Cooled Pintle and Water Flow Test of Cooling Channels

 


50

Á¤¹Î±Ô Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø(KARI)

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú ¼®»ç('25.02)

- Labview ÄÚ¾î 2(Áß±Þ) ±³À° (2023.08)
 

Master Thesis

3 tonf±Þ ¸Þź¿¬·á »ó´Ü ¿£ÁøÀÇ Àü±âÆßÇÁ ¼º´É Ư¼º ¿¬±¸

 

Hydraulic Performance Evaluation of the 3-tonf Thrust Class ElecPump for a Liquid Methane Upper Stage Rocket Engine

 


51

À°»ó¿ì(ÆÄÆ® ŸÀÓ ¼®»ç) Æ丮Áö¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú ¼®»ç('25.02)


 

Master Thesis

¼ÒÇü¹ß»çü ÃßÁøÁ¦ ÅÊÅ© °æ·®È­¸¦ À§ÇÑ CFRP-±Ý¼Ó °áÇպΠ´©¼³ ¾ïÁ¦ ¼³°è ¿¬±¸

 

Study on the design of CFRP-metal joint leakage suppression for the weight reduction of a small launch vehicle propellant tank

 


 

ÀüÀÓ¿¬±¸¿ø (Researcher)

 

Ȳ±â¿µ ±¹¹æ°úÇבּ¸¼Ò(ADD)

- ±¹¹æ°úÇבּ¸¼Ò(ADD) ¿¬/¼±ÀÓ/Ã¥ÀÓ/¼ö¼®¿¬±¸¿ø('79.12~'19.09)
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú °âÀÓ±³¼ö('16.03~'18.02)
- Çѱ¹ÃßÁø°øÇÐȸ ÀÌ»ç/°¨»ç, ´Ü±â°­Á Á¶Á÷À§¿øÀå, ·¥/½ºÅ©·¥Á¦Æ®ÃßÁø ºÎ¹®À§¿øÀå('12.01~)
- Çѱ¹±º»ç°úÇбâ¼úÇÐȸ(ÃßÁøºÎ¹®) ºÎ¹®À§¿ø/ÆíÁýÀ§¿ø('15.01~)
- ±¹°¡°úÇбâ¼úÀÚ¹®È¸ÀÇ(½ÉÀÇȸÀÇ) °ø°ø¿ìÁÖÀü¹®À§¿øȸ Àü¹®À§¿ø, ¿ìÁÖÇ×°ø¼ÒÀ§¿øÀå('19.01~)

- ¿¬¼¼´ëÇб³ ±â°è°øÇаú ¹Ú»ç('94.08)
- ¿¬¼¼´ëÇб³ ±â°è°øÇаú ¼®»ç('86.08)

 


 

 

¹Ú»ç ÈÄ ¿¬¼ö (Post-Doctor)

ÁغñÁßÀÔ´Ï´Ù.

±Ç¹ÎÂù ±¹¹æ°úÇבּ¸¼Ò(ADD)

- ·¯½Ã¾Æ MAI ¹Ú»ç
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ Çлç

   

 

 

Çлç (Bachelor)

ÁغñÁßÀÔ´Ï´Ù.

°øµµ¿¬ Çö´ëÁß°ø¾÷(ÁÖ)
doyoun.kong@doosan.com
- Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇÐ Çлç
 

   


   Webadmin : Hyunjin Jeong (disneyboy@naver.com)

High speed Propulsion and Combustion Laboratory : HPCL

Copyright(c) All rights reserved.