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´ëÀü±¤¿ª½Ã À¯¼º±¸ ´ëÇзΠ99
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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


International Conference

Effect of Scale on the performance of Heat-Recirculating Reactors

 

2006.06.

4th International Energy Conversion Engineering Conference and Exhibit(IECEC)

 

Effect of Geometry and Scale on the Performance of Swiss-roll combustor for Micro Power Generation

  2006.08.

The Combustion Institute 31st International Symposium, Germany

 

Effect of Scale and geometry on the performance of Heat-Recirculating Swiss roll comnbustors

  2007.05.

6th Asia-Pacific conference on Comnbustion pp.538~541

 


 

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 žÀçǰ¿¡ ¿­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

Ãʰí¼Ó 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 ÇÉÆ² 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


International Conference

Measured Characteristics of Flow and Combustion in Supersonic Flame/Shock Wave Interaction

  2001.07.

Proceedings of the Third Asia-Pacific Conference on Combustion pp.714~717

 

Assessment of Thrust From Pressure Measurement of Supersonic Combusto

 

2002.07.

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibi

 

 

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

Aboard Conference

Preliminary Experiment for Micro Propulsion Device

 

2004.10

Asian Joint Conference on Propulsion and Power

 


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


International Conference

Characteristic Study of Micro-Nozzle Performance and Thermal Transpiration Based Self Pumping in Vacuum Conditions

  2007.04.

JSASS-KSAS Joint International Symposium on Aerospace Engineering pp.208~215

Characteristic Study of Micro-Nozzle Performance and Thermal Transpiration Based Self Pumping in Vacuum Conditions

2008.03.

Asian Joint Conference on Propulsion and Power

 


 

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


International Conference

Effect of Scale and fuel type on heat-recirculation combustor performance

  2007.03.

5th US Combustion Meeting Organized by the Western States Section of the Combustion Institute and Hosted by the University of California at San Diego

 


 

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× ÆØÃ¢ºñ 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 ÇÃ¶ó½ºÆ½ ¿¬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 ÇØ¼®

 

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 ÇÉÆ² ³ëÁñÀÇ ¼öÄ¡ÇØ¼®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¸¦ Ȱ¿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±â¼úǰÁú¿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× Ȱ¿ë ´Ü±â°­Á (2010. 08)
- Fluent Turbulence °úÁ¤ (2011. 01)
- Fluent Heat Transfer °úÁ¤ (2011. 02)
- Ansys Combustion ±³À° (2011. 05)

Master Thesis

ÇÉÆ²±¸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× Ȱ¿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

ÇÉÆ²ÀÌ ±¸µ¿ÇÏ´Â ³ëÁñÀÇ ¼öÄ¡ÇØ¼®Àû °ËÁõ ¿¬±¸

 

Computational Analysis of Pintle Driven Nozzle

 


28

±èµ¿¿¬ ÆÛ½ºÅØ(ÁÖ) -> (ÁÖ)À¯¾ÆÀÌÆ¼ -> (ÁÖ)ŰÇÁÄÚÀüÀÚÇ×°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 ÇÉÆ² 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

ÇÉÆ² 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

Ãʰí¼Ó 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 ÇÉÆ² Ã߷±⠽ýºÅÛ¿¡ °üÇÑ ¼öÄ¡Àû ¿¬±¸

 

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


International Conference

Analytical Study of Drive Mechanism for Multi-axis Pintle Thrusters

 

2016.03

Proceedings of the Asian Joint Conference on Propulsion and Power 2016, AJCPP2016-090

   

Fundamental Experiment of a Plasma Generator for Drag Reduction Applications

  2016.06.

Conference Proceedings Europe-Korea Conference on Science and Technology 2016, EKC2016-085

   

Analytical Study on Two-axis Pintle Thrusters with Coupling Drive Mechanism

  2016.06

Conference Proceedings Europe-Korea Conference on Science and Technology 2016, EKC2016-163

   

Analysis of Injection Conditions of Counterflow Jets for Drag Reduction of a High Speed Vehicle

  2018.03.

2018 the Asian Joint Conference on Propulsion and Power, AJCPP2018-05

   

A Study of Steady Characteristics on Two-Axis Pintle Thrusters with the Different Pintle Shap

  2018.08.

Conference Proceedings Europe-Korea Conference on Science and Technology 2018, EKC2018-MA-04

   

Effect of Nozzle Geometry on Counterflow Jets for Drag Reduction of a High Speed Vehicle

  2018.10.

69th International Astronautical Congress 2018

   

Fundamental Experiment on Actuators for Two-Axis Pintle Thrusters

  2019.08

Conference Proceedings Europe-Korea Conference on Science and Technology 2019

   

A Study of Unsteady Characteristics on Two-axis Pintle Thrusters with the Different Pintle Shape

  2019.08

Conference Proceedings US-Korea Conference on Science, Technology and Enterpreneurship 2019

   

Experimental Investigation on Darg Reduction by Plasma Counterflow Jets in Mach 7 Shock Tunnel

  2019.10.

70th International Astronautical Congress 2019

 


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 ÇÉÆ² Ã߷±âÀÇ ºñÁ¤»ó»óÅ Ư¼º ¹× ¿ÜºÎÇü ÇÉÆ² 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

ÇÉÆ² 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


International Conference  

Effect of Inflection Angle on Transition Characteristics of Dual Bell Nozzles

  2016.06.

Conference Proceedings Europe-Korea Conference on Science and Technology 2016, EKC2016-164

   

Transition Characteristics of Dual Bell Nozzles with Extension Length

  2016.06.

Conference Proceedings Europe-Korea Conference on Science and Technology 2016, EKC2016-165

 


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


International Conference  

Fundamental Experiment of a Plasma Generator for Drag Reduction Applications

  2016.06.

Conference Proceedings Europe-Korea Conference on Science and Technology 2016, EKC2016-085

   

Construction of Fundamental Experiment System of a Plasma Generator for Drag Reduction Research

  2017.07.

Conference Proceedings Europe-Korea Conference on Science and Technology 2017, EKC2017

     

 


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


International Conference  

Performance Analysis of an Expansion-Deflection Nozzle According to Initial Angle of a Pintle

  2017.07.

Conference Proceedings Europe-Korea Conference on Science and Technology 2017, EKC2017

   

Evaluation of Payload Gain according to E-D Nozzle Length Reduction

    2017.10.

2017 Aisa-Pacific International Symposium on Aeroapace Technology, APISAT2017-C6-1


 

37

¹Ú»óÇö ±¹¹æ±â¼úÁøÈ↓±¸¼Ò(KRIT) -> ±¹¹æ°úÇבּ¸¼Ò(ADD)
 
- 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


International Conference  

Experimental Study of Flow Characteristics in an Expansion-Deflection Nozzle at Low Nozzle Pressure Ratios

  2017.07

Conference Proceedings Europe-Korea Conference on Science and Technology 2017, EKC2017

 


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


International Conference  

Fundamental Experiments on Temperature Measurements of a Plasma Jet

  2017.07.

Conference Proceedings Europe-Korea Conference on Science and Technology 2017, EKC2017

 


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 ÇÉÆ² 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


International Conference  

A Study on Internal Flow Field of External Pintle Nozzle with the Different Nozzle Throat Angle

  2018.08.

Conference Proceedings Europe-Korea Conference on Science and Technology 2018, EKC2018-MA-03

   

Design of External Pintle Nozzle with Pintle Injector for Methane Rocket Engine

  2019.08.

Conference Proceedings Europe-Korea Conference on Science and Technology 2019

   

A Numerical Study on the Variation of Internal Flow Field of the External Pintle Nozzle with Pintle Radius

  2019.09.

Conference Proceedings Europe-Korea Conference on Science and Technology 2019

 


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


International Conference

Experiments of Counterflow Jets using Air and Plasma Injection according to Mach Number of Nozzle Exit

  2018.08.

Conference Proceedings Europe-Korea Conference on Science and Technology 2018, EKC2018-MA-05

 

Characteristics of Supersonic Diffuser with Constant Circular Cross Section

  2019.08.

Conference Proceedings Europe-Korea Conference on Science and Technology 2019

   

Parametric Studies of Diffuser for Constant Test Section Mach Number in Free-jet Supersonic Wind Tunnel

  2019.08.

The 10th Asian-Pacific Conference on Aerospace Technology and Science & The 4th Asian joint Symposium on Aerospace Engineering

   

Preliminary Design of High Speed Test Facility for Counterflow Jet Experiments Reducing Heat and Drag

  2019.10.

70th International Astronautical Congress 2019

 


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


International Conference

Fundamental Numerical Study for Performance of an Expansion-Deflection Nozzle according to the Base Nozzle Length

  2019.08.

Conference Proceedings Europe-Korea Conference on Science and Technology 2019

   

Experimental Study on an Expansion-Deflection Nozzle Characteristics according to the Pintle Inflection Angle

  2019.08.

Conference Proceedings US-Korea Conference on Science, Technology and Enterpreneurship 2019

   

Fundamental Numerical Study for Performance of E-D Rocket Nozzle according to the Pintle Design Parameters

  2019.08.

The 10th Asian-Pacific Conference on Aerospace Technology and Science & The 4th Asian joint Symposium on Aerospace Engineering

 


42

¹é°æ¹Ì ±¹¹æ±â¼úÁøÈ↓±¸¼Ò(KRIT) -> ±¹¹æ±â¼úǰÁú¿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±âÀåÇØ¼® ±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


International Conference

Conceptual Design on Main Components of the Electric-Pump Cycle Engine

  2019.08.

Conference Proceedings Europe-Korea Conference on Science and Technology 2019

   

Research Trends of Electric-Pump Cycle for Liquid Rocket Engines in Republic of Korea

  2019.08.

Conference Proceedings US-Korea Conference on Science, Technology and Enterpreneurship 2019

   

Fundamental Tests of the Propellant Supply System of the Electric-pump Cycle for Space Propulsion Systems

  2021.03.

10th Asian Joint Conference on Propulsion and Power 2021


44

±è°Ç¿µ ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ) ±¹¹æ°úÇבּ¸¼Ò(ADD)  

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


International Conference

Components Design of an Experimental System for a Lab-Scaled Electric Pump-fed Cycle

  2021.11.

Asia-Pacific International Symposium on Aerospace Technology 2021

 

Evaluation of a Space-borne MLI Performance by Using an Experimental Estimation

  2022.06.

32nd International Symposium on Rarefied Gas Dynamics

 

Experimental Estimation of the Effective Emissivity of a Space-borne MLI Based on Design Parameters

  2022.07.

9th European Conference for Aeronautics and Space Sciences(EUCASS 2022)

 

Simulation Study of an Electric Pump-fed Cycle Flow Characteristics by Using a 1-D Modeling Analysis

  2022.10.

Asia-Pacific International Symposium on Aerospace Technology 2022

 


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


International Conference

Thrust Analysis by Length Reduction of an ED Nozzle with Fixed Expansion Ratio

 

2022.07.

9th European Conference for Aeronautics and Space Sciences(EUCASS 2022)

 


46

±èÁذâ ÷´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


International Conference

Mass Estimation of an Electric Pump Cycle Engine for 30kN-class Upper Stage Launch Vehicle Based on a Battery Technology

  2022.07.

9th European Conference for Aeronautics and Space Sciences(EUCASS 2022)

 

Battery Mass Estimation of an Electric Pump Cycle for Upper-Stage Propulsion Systems

  2023.03.

11th Asian Joint Conference on Propulsion and Power 2023

 


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


International Conference

Environmental Test of Lithium-ion Batteries for Electric Pump-fed Systems Applications

  2023.03.

11th Asian Joint Conference on Propulsion and Power 2023

   

Development of Vacuum Facility for evaluating Battery Discharge Characteristics in High Altitude Environments

  2023.08.

Conference Proceedings Europe-Korea Conference on Science and Technology 2023

   

A study on the performance of lithium-ion batteries according to altitude

  2024.07.

Europe-Korea Conference on Science and Technology 2024

 

 


48

¿°°æÈÆ(ÆÄÆ® ŸÀÓ ¼®»ç) Æä¸®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


International Conference

Construction of a Bipropellant Water Flow Test Apparatus Applied with an Electric Pump-fed Cycle

  2023.08.

Conference Proceedings Europe-Korea Conference on Science and Technology 2023

 

Applicability of an Electric Pump-fed Cycle Engine for Satellite Thruster

 

2024.05.

Space Propulsion Conference 2024

Research Trends in Electric Pump-fed Cycle Engines from 2020 to 2024

2024.10.

Asia-Pacific International Symposium on Aerospace Technology 2024

 


50

ÀÌâÁ¾ ¹Ì·¡¸ðºô¸®Æ¼½Ã½ºÅÛ¿¬±¸¼Ò -> ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

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 ÇÉÆ²ÀÇ ¿­À¯µ¿ ÇØ¼® 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


International Conference

Analysis of Cooling Performance according to the Thickness of the Pintle Outer Wall

  2023.08.

Conference Proceedings Europe-Korea Conference on Science and Technology 2023

   

Heat Transfer Characteristics of Regenerative Cooling for an ED Nozzle Pintle

  2024.10.

Asia-Pacific International Symposium on Aerospace Technology 2024

 


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 ¿£Áø¿ë Àü±âÆßÇÁÀÇ ¼º´É Æò°¡

 

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


International Conference

Preliminary Design of an Electric Pump-Fed Cycle for a Methane Upper Stage Engine Based on a 1-D Simulation Analysis

  2023.08.

Conference Proceedings Europe-Korea Conference on Science and Technology 2023

 


51

À°»ó¿ì(ÆÄÆ® ŸÀÓ ¼®»ç) Æä¸®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

 


52

ÀÌÁ¤Ç× ÇÑÈ­¿¡¾î·Î½ºÆäÀ̽º(ÁÖ)

Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú ¼®»ç('25.08)

-ANSYS Fluent Basic (2023.02.)

-ANSYS Mechanical Basic (2023.02.)

-ANSYS Chemkin-Pro (2024.04.)
 

Master Thesis

ºÐ»ç °¡½º¿¡ µû¸¥ ¿ªºÐ»ç Á¦Æ®ÀÇ À¯µ¿ Ư¼º ºÐ¼® ¿¬±¸

 

A Study on the Flow Characteristics of Counterflow Jets According to Injection Gas


International Conference

Analysis of the Structural Effect of Aerodynamic Loads on the ED Nozzle Pintle

  2023.08.

Conference Proceedings Europe-Korea Conference on Science and Technology 2023

 


 

 

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§¿øÈ¸ 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
 

   


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