sub menu
gadget
[ 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
Hydraulic Performance of the Liquid Methane Electric Pump Under Deign and Off-Deign Conditions
Mingyu Jeong, Hyun-Duck Kwak, Hawnil Huh
International Journal of Aeronautical and Space Sciences(IJASS) Åõ°í
ȼº Âø·ú¼±ÀÇ ÁøÀÔ, ÇÏ° ¹× Âø·ú(EDL) °úÁ¤¿¡ ´ëÇÑ ±â¼ú ¹× ¿¬±¸ µ¿Çâ (Part 1 : Entry, Landing, and GN&C)
Technology and Research Trends on Entry, Descent, and Landing(EDL) Process of Mars Landers (Part 1 : Entry, Landing, and GN&C)
¼ÕÁßÈÆ, ÀÌÁ¤Ç×, ÀÌÁÖ¹Ì, ÇãȯÀÏ
2025. 02.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 53±Ç Á¦ 2È£ pp.219-237
Àü±âÆßÇÁ »çÀÌŬ°ú ED ³ëÁñÀ» Àû¿ëÇÑ ¹ß»çü »ó´ÜÀÇ Áß·® ÃßÁ¤ ¿¬±¸
Study on Estimating the Mass of the Upper Stage of a Launch Vehicle Using Electric Pump Cycle and an ED Nozzle
±èÁØ°â, ±è°Ç¿µ, ÀÌÁÖ¹Ì, À̹ÎÈ£, Á¤¹Î±Ô, ÀÌÇüÁø ÇãȯÀÏ
2024. 05.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 52±Ç Á¦ 5È£ pp. 401-413
Ç×°ø¿ìÁÖ ±â¼ú¿¡ ¸®Æ¬ÀÌ¿Â ¹èÅ͸® Àû¿ëÀ» À§ÇÑ ¿ä±¸ Á¶°Ç°ú ÃֽŠµ¿Çâ
Requirements and Trends for the Application of Lithium-Ion Battery in Aerospace Technology
À̹ÎÈ£, ¼ÕÁßÈÆ, ÇãȯÀÏ
2024. 03.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 52±Ç Á¦ 3È£ pp. 209-223
»ó´Ü ¾×ü·ÎÄÏ¿£Áø¿ë Åͺ¸ÆßÇÁ ½ÃÇèÀ» À§ÇÑ Åͺ󱸵¿½Ã½ºÅÛ °³¹ß½ÃÇè
Development Test on the Turbine Drive System of Turbopump Test for Upper Stage Liquid Rocket Engines
¿Õ½Â¿ø, ±èÁø¼±, ½É¸íº¸, ±è´ëÁø, ÇãȯÀÏ
2024. 02.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 28±Ç Á¦ 1È£ pp. 67-76, 2024
Evaluation of Effective Emissivity Based on Manufacturing and Mounting Scheme for Space-borne Multilayer Insulation
Jungyeom Kim, Jin-Soo Chang, Geon Young Kim, Hwanil Huh
2024. 03.
Journal of Mechanical Science and Technology ,Vol. 38, pp. 1497-1506, 2024
Experimental Study on Flow Control System of an Electric Pump-Fed Cycle for Thrust Contro l
Geon Young Kim, Hyoung Jin Lee, Hwanil Huh
2024. 03.
Acta Astronautica . V ol. 2 16, p p. 44-56
Performance Analysis of an E xpansion- D eflection N ozzle with Reduced Lengths of Nozzle Extension at a
High-Altitude Environment
Joomi Lee, Junsub Choi, Hwanil Huh
2023. 10.
Journal of Mechanical Science and Technology, 37, pp. 6547-6558, 2023
¹èÅ͸® ±â¼ú ¹ßÀü µ¿Çâ°ú Ç×°ø ¿ìÁÖ ÀÓ¹«ÀÇ Àü±â±¸µ¿ ½Ã½ºÅÛ (PART 2 : ¿ìÁÖ ºÐ¾ß Àü±â±¸µ¿ ½Ã½ºÅÛÀÇ ¹èÅ͸® È°¿ë)
Development Trends of Battery Technologies and Electrical-driven System for Aerospace Missions (PART 2 : Battery Utilization in Electrical-driven System for Space Missions)
±è°Ç¿µ, ÀÌÇüÁø, À̹ÎÈ£, ÇãȯÀÏ
2023. 10.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 51±Ç Á¦ 10È£ pp. 709-719
¹èÅ͸® ±â¼ú ¹ßÀü µ¿Çâ°ú Ç×°ø ¿ìÁÖ ÀÓ¹«ÀÇ Àü±â±¸µ¿ ½Ã½ºÅÛ (PART 1 : ¸®Æ¬°è¿ ¹èÅ͸® ¹× Àü±âÃßÁø Ç×°ø±â °³¹ß µ¿Çâ)
Development Trends of Battery Technologies and Electrical-driven System for Aerospace Missions (PART 1 : Development Trends of Lithium based Batteries and Electrified Aircraft Propulsion System)
±è°Ç¿µ, ÀÌÇüÁø, ±èÁØ°â, ÇãȯÀÏ
2023. 10.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 51±Ç Á¦ 10È£ pp. 693-708
Development Trend of Liquid Hydrogen-Fueled Rocket Engines (Part 2: Core technologies)
Donghwi Ha, Tae-seong Roh, Hwanil Huh, Hyoung Jin Lee
International Journal of Aeronautical and Space Sciences(IJASS), Vol. 24, pp. 146-165
2023. 08.
https://doi.org/10.1007/s42405-022-00518-8
Development Trend of Liquid Hydrogen-Fueled Rocket Engines (Part 1: Performance and Operation)
Donghwi Ha, Tae-seong Roh, Hwanil Huh, Hyoung Jin Lee
International Journal of Aeronautical and Space Sciences(IJASS), Vol. 24, pp. 131-145
2023. 08.
https://doi.org/10.1007/s42405-022-00519-7
³ëÁñ ±æÀÌ ´ÜÃà ¹æ¾È¿¡ µû¸¥ ED ³ëÁñÀÇ ¼º´É ºÐ¼®
Performance Analysis of an Expansion Deflection Nozzle by Nozzle Length Reduction Method
ÀÌÁÖ¹Ì, ÃÖÁؼ·, ÇãȯÀÏ
2022. 10.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 26±Ç Á¦ 5È£ pp. 11-23
Performance analysis of an expansion-deflection(E-D) nozzle based on pintle inflection angle
Junsub Choi, Hwanil Huh
2022. 10.
Journal of Mechanical Science and Technology, Vol. 36, No. 12
Development of Ultra Low Specific Speed Centrifugal Pumps Design Method for Small Liquid Rocket Engines
Hye in Kim, Tae-seong Roh, Hwanil Huh, Hyoung Jin Lee
Aerospace 2022, 9, 9, 477
2022. 08.
https://doi.org/
10.3390/aerospace9090477
Àü±âÆßÇÁ »çÀÌŬ ¿ìÁÖÃßÁø ÀåÄ¡ÀÇ ¹ëºê ¹× ÆßÇÁ ȸÀü¼ö Á¶Àý¿¡ µû¸¥ Á¤Àû À¯·® °ø±Þ Ư¼º
Static Flow Characteristics of an Electric Pump-fed Cycle Space Propulsion System Using a Valve and Pump RPM Control
±è°Ç¿µ, ÀÌÇüÁø, ±èÁØ°â, ÇãȯÀÏ
2022. 09.
´ëÇѱâ°èÇÐȸ ³í¹®Áý B±Ç Á¦ 46±Ç Á¦ 9È£ pp. 515-527
¿ìÁֹ߻çü »ó´Ü ¿£Áø °³¹ß µ¿Ç⠺м®
Trend Analysis in Upper Stage Engine Development of Space Launch Vehicles
ÇÑ°æȯ, ³ëżº, ÇãȯÀÏ, ÀÌÇüÁø
2022. 04.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 26±Ç Á¦ 2È£ pp. 79-95
±â°è½Ä ÃßÁø ½Ã½ºÅÛ Á¦¾î¸¦ À§ÇÑ °¡½ºÅÍºó ¿£Áø ¸ðµ¨¸µ ¹× ½Ã¹Ä·¹À̼Ç
Modeling and Simulation of a Gas Turbine Engine for Control of Mechanical Propulsion Systems
¹é°æ¹Ì, ÇãȯÀÏ, ±âÀÚ¿µ
2021. 08.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 25±Ç Á¦ 4È£ pp. 43-52
¼±¹Ú¿ë MT30 °¡½ºÅÍºó ¿£ÁøÀÇ ¼º´É ¸ðµ¨¸µ¿¡ °üÇÑ ¿¬±¸
Study on Performance Modeling of a MT30 Gas Turbine Engine for Marine Ship Applications
¹é°æ¹Ì, ±âÀÚ¿µ, ÇãȯÀÏ
2021. 02.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 25±Ç Á¦ 1È£ pp. 12-18
Àü±âÆßÇÁ »çÀÌŬÀÇ ÃßÁøÁ¦ °ø±Þ ½Ã½ºÅÛ ¸ð»ç¿ë ¼ö·ù ½ÃÇè ¿¬±¸
A Study on Water Flow Test for Simulating Propellant Supply System of Electric Pump Cycle
±â¿ø±Ù, Ȳ±â¿µ, ÀÌÀçû, ÃÖÁؼ·, ÇãȯÀÏ, ±è°Ç¿µ
2021. 02.
´ëÇѱâ°èÇÐȸ ³í¹®Áý B±Ç Á¦ 45±Ç Á¦ 2È£ pp.115-124
¾×ü ÃßÁøÁ¦ °ø±Þ ½Ã½ºÅÛÀÇ Á¤Æ¯¼º ¸ðµ¨¸µ ¹× °ËÁõ
Modeling and Validation of a Liquid Propellant Supply System in Steady States
ÀÌÁÖ¿¬, ±â¿ø±Ù, ÇãȯÀÏ, ³ëżº, ÀÌÇüÁø
2020. 12.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 24±Ç Á¦ 6È£ pp. 143-154
¸¶ÇÏ 7 ±ØÃÊÀ½¼Ó Ãæ°ÝÆÄ Åͳο¡¼ Ç×·Â °¨¼Ò¸¦ À§ÇÑ ÇöóÁ Á¦Æ® ¹ß»ýÀåÄ¡ ¿¬±¸
A Study on Plasma Jet Generator in a Mach 7 Hypersonic Shock Tunnel for Drag Reduction Applications
ÀÌÀçû, ÀÌÀ¯¼®, ÀÌÇüÁø, ÇãȯÀÏ
2020. 11.
´ëÇѱâ°èÇÐȸ ³í¹®Áý B±Ç Á¦ 44±Ç Á¦ 11È£ pp. 663-671
¼ÒÇü¹ß»çü °³¹ß ¹× ÃֽŠ±â¼ú µ¿Çâ
Technology and Development Trends of Small Launch Vehicles
ÃÖÁؼ·, ÇãȯÀÏ, ±â¿ø±Ù
2020. 10.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 24±Ç Á¦ 5È£ pp. 91-102
Performance Analysis and Mass Estimation of a Small-Sized Liquid Rocket Engine with Electric-Pump Cycle
Juyeon Lee, Tae-seong Roh, Hwanil Huh, Hyoung Jin Lee
International Journal of Aeronautical and Space Sciences(IJASS)
2020. 10.
https://doi.org/10.1007/s42405-020-00325-z
±ØÃÊÀ½¼Ó È°°ø ºñÇàü(HGV)ÀÇ ¿¬±¸°³¹ß µ¿Çâ
Research and Development Trends of a Hypersonic Glide Vehicle (HGV)
Ȳ±â¿µ, ÇãȯÀÏ
2020. 09
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 48±Ç Á¦ 9È£ pp. 731-743
Drag Reduction Analysis of Counterflow Jets in a Short Penetration Mode
Jaecheong Lee, Hyoung Jin Lee, Hwanil Huh
Aerospace Science and Technology Vol. 106
2020. 07.
https://doi.org/10.1016/j.ast.2020.106065
Çѱ¹Çü¹ß»çü¸¦ ±â¹ÝÀ¸·Î ÇÑ ·ÎÄÏ ³ëÁñÀÇ µ¿°á ¹× ÆòÇü À¯µ¿ Çؼ® °á°ú¿¡ µû¸¥ ¼º´É Ư¼º
Performance Characteristics of a Rocket Nozzle Based on the KSLV-II According to the Results of Frozen and Equilibrium Flow Analysis
¹®Å¼®, ±èÇѼÖ, ÇãȯÀÏ
2020. 03
´ëÇѱâ°èÇÐȸ ³í¹®Áý B±Ç Á¦ 44±Ç Á¦ 3È£ pp. 161-168
Study on the Combined Effect of Various Injection Conditions on the Drag Reduction by a Counter-flow Jet in Supersonic Flow
Yongchan Kim, Tae-Seong Roh, Hwanil Huh, Hyoung Jin Lee
2020. 03.
Aerospace Science and Technology Vol. 98
https://doi.org/10.1016/j.ast.2019.105580
»ó´Ü ÃßÁø ½Ã½ºÅÛ¿¡ Àû¿ëÀ» À§ÇÑ Àü±âÆßÇÁ »çÀÌŬÀÇ ±¹¿Ü ¿¬±¸ µ¿Çâ
Overseas Research Trends of an Electric-Pump Cycle for Application in Upper-Stage Propulsion Systems
±â¿ø±Ù, ÀÌÀçû, ÀÌÇüÁø, ³ëżº, ÇãȯÀÏ
2020. 02.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 24±Ç Á¦ 1È£ pp. 64-77
¾×ü ÃßÁøÁ¦ °ø±Þ ½Ã½ºÅÛÀÇ ¸ðµ¨¸µ ¹× ½Ã¹Ä·¹ÀÌ¼Ç ¿¬±¸ µ¿Ç⠺м®
Research Trend Analysis on Modeling and Simulation of Liquid Propellant Supply System
ÀÌÁÖ¿¬, Â÷½Â¿ø, Çϵ¿ÈÖ, ±â¿ø±Ù, ÀÌÀçû, ÇãȯÀÏ, ³ëżº, ÀÌÇüÁø
2019. 12.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 23±Ç Á¦ 6È£ pp. 39-50
¹ß»çüÀÇ °íµµº¸Á¤¿ë 3D ÇÁ¸°Æà ȮÀå-±¼Àý ³ëÁñ¿¡ °üÇÑ ½ÇÇèÀû ¿¬±¸
Experimental Study on a 3D Printed Altitude-Compensating Expansion-Deflection Nozzle for a Launch Vehicle
À̱âȯ, ¹Ú»óÇö, ±¸ÀÚ¿¹, ÇãȯÀÏ
2019. 12.
´ëÇѱâ°èÇÐȸ ³í¹®Áý B±Ç Á¦ 43±Ç Á¦ 12È£ pp. 859-869
°¡º¯ ÇÉƲ ÀÎÁ§ÅÍ¿¡¼ ÇÉƲ ÆÁ Çü»ó¿¡ µû¸¥ ºÐ¹«Æ¯¼º ¿¬±¸
Spray Characteristics of a Movable Pintle Injector with Pintle Tip Shape
³²Á¤¼ö, ÀÌ°Ç¿õ, ¹Ú¼±Á¤, ÇãȯÀÏ, ±¸ÀÚ¿¹
2019. 09
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 47±Ç Á¦ 9È£ pp. 658-664
ÇÉƲ º¯°î °¢µµ¿¡ µû¸¥ E-D ³ëÁñ Ư¼º¿¡ ´ëÇÑ Àü»ê¼öÄ¡Çؼ® ¿¬±¸
Numerical Study on an E-D Nozzle Characteristics with Various Pintle Inflection Angles
¹Ú»óÇö, ¹®Å¼®, ÇãȯÀÏ
2018. 12.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 22±Ç Á¦ 6È£ pp. 19-27
°íµµº¸Á¤ ³ëÁñÀÇ ±â¼ú ¹× ƯÇã µ¿Çâ
Technology and Patent Trends of Altitude Compensation Nozzles
ÃÖÁؼ·, ¹®Å¼®, ÃÖÁ¾ÀÎ, ¹Ú»óÇö ±èÇѼÖ, ÇãȯÀÏ
2018. 08
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 46±Ç Á¦ 8È£ pp. 662-670
µà¾ó º§ ³ëÁñÀÇ ¼³°è º¯¼ö¿¡ µû¸¥ õÀÌ Æ¯¼º
Transition Characteristics with Design Parameters of Dual Bell Nozzle
±èÁ¤ÈÆ, ÇãȯÀÏ
2018. 07.
´ëÇѱâ°èÇÐȸ³í¹®Áý B±Ç Á¦ 42±Ç Á¦7È£ pp. 503-511
1-D ½Ã¹Ä·¹À̼ÇÀ» È°¿ëÇÑ 2Ãà ÇÉƲ Ã߷±⠽ýºÅÛÀÇ ¾Ð·Â°ÇÏ Æ¯¼º ºÐ¼®
Analysis of Pressure Drop in Two-Axis Pintle Thrusters Using 1-D Simulation
ÀÌÀçû, ÇãȯÀÏ
2018. 03.
´ëÇѱâ°èÇÐȸ³í¹®Áý B±Ç Á¦ 42±Ç Á¦ 3È£ pp. 177-186
ÃÊÀ½¼Ó ȯ°æ¿¡¼ ¿ªºÐ»ç °ø±â Á¦Æ®ÀÇ ¾Ð·Â º¯È¿¡ µû¸¥ À¯µ¿ Ư¼º ¹× Ç×·Â °¨¼Ò
Flow Characteristics and Drag Reduction with Different Pressures of Counterflow Air Jets in Supersonic Flow
ÃÖÁ¾ÀÎ, ÀÌÀçû, °½Â¿ø, ÇãȯÀÏ
2018. 02.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 22±Ç Á¦ 1È£ pp. 58-65
µà¾ó º§ ³ëÁñ°ú E-D ³ëÁñÀ» °áÇÕÇÑ Çѱ¹Çü¹ß»çüÀÇ ºñÃß·Â Áõ°¡
Specific Impulse Gain for the KSLV-II with Combination of Dual Bell Nozzle and E-D Nozzle
¹®Å¼®, ÇãȯÀÏ
2018. 02.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 22±Ç Á¦ 1È£ pp. 16-27
ÇöóÁ ºÐ»çÀåÄ¡¸¦ È°¿ëÇÑ ÃÊ°í¼Ó ºñÇàüÀÇ Ç׷°¨¼Ò ±âÃÊ ½ÇÇè
Fundamental Experiments of Drag Reduction for a High Speed Vehicle Using Plasma counterflow Jets
°½Â¿ø, ÃÖÁ¾ÀÎ, ÀÌÀçû, ÇãȯÀÏ
2017. 12.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 21±Ç Á¦ 6È£ pp.57-63
°íµµ º¸Á¤¿ë È®Àå-±¼Àý(E-D) ³ëÁñÀÇ ±¹¿Ü ¿¬±¸ µ¿Çâ
Research Trends of an E-D Nozzle for Altitude Compensation
¹®Å¼®, ¹Ú»óÇö, ÃÖÁؼ·, ÇãȯÀÏ
2017. 10.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 45±Ç Á¦ 10È£ pp.844-854
ÆØâºñ°¡ °íÁ¤µÈ µà¾ó º§ ³ëÁñÀÇ ÃµÀÌƯ¼º¿¡ ´ëÇÑ ¼öÄ¡Çؼ® ¿¬±¸
Numerical Study on Transition Characteristics of Dual Bell Nozzle with Expansion Ratio Fixed
ÃÖÁؼ·, ÇãȯÀÏ
2017. 06.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 21±Ç Á¦ 3È£ pp.68-75
³ëÁñ ¸ñ ³»ºÎÇü ÇÉƲÃ߷±âÀÇ Ãß·Â ¹× °ø·ÂÇÏÁß Æ¯¼º
Thrust and Aerodynamic Load Characteristics of an Internal Pintle Thruster
ÃÖÁؼ·, ±èµ¿¿¬, ÇãȯÀÏ
2017. 06.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 21±Ç Á¦ 3È£ pp.1-9
Reduced Actuator Set for Pressure Control and Thrust Distribution for Multinozzle Propulsion Systems
Yeerang Lim, Jaecheong Lee, Hyochoong Bang, Hwanil Huh, Hosung Lee
2017. 05.
International Journal of Aerospace Engineering Vol.2017
https://doi.org/10.1155/2017/4104212
Numerical Study for Flame Deflector Design of a Space Launch Vehicle
Hwayoung Oh, Jungil Lee, Hyungsik Um, Hwanil Huh
2017. 04.
Advances in Space Research Vol.59 No.7 pp.1833~1847
https://doi.org/10.1016/j.asr.2016.12.038
ÃÊ°í¼Ó ºñÇàü Ç×·Â °¨¼Ò¸¦ À§ÇÑ ÇöóÁ ºÐ»çÀåÄ¡¿¡ ´ëÇÑ ¿¹ºñ °á°ú
Preliminary Results on Plasma Counterflow Jets for Drag Reduction of a High Speed Vehicle
°½Â¿ø, ÃÖÁ¾ÀÎ, ÀÌÀçû, ÇãȯÀÏ
2016. 12.
Çѱ¹ÃßÁø °øÇÐȸÁö Á¦ 20±Ç Á¦ 6È£ pp.101-112
Çѱ¹Çü¹ß»çü¸¦ ±â¹ÝÀ¸·Î ÇÑ µà¾ó º§ ³ëÁñÀÇ Àü»ê¼öÄ¡Çؼ® ±âÃÊ °á°ú
Preliminary CFD Results of a Dual Bell Nozzle based on the KSLV-II
±èÁ¤ÈÆ, ÃÖÁؼ·, ÇãȯÀÏ
2016. 12.
Çѱ¹ÃßÁø °øÇÐȸÁö Á¦ 20±Ç Á¦ 6È£ pp.18-28
°íµµ º¸Á¤¿ë E-D ³ëÁñÀÇ Ã߷ Ư¼º¿¡ ´ëÇÑ ¼öÄ¡Çؼ® ¿¬±¸
Numerical Study on Thrust Characteristics of an E-D Nozzle for Altitude Compensation
ȲÈñ¼º, ÇãȯÀÏ
2016. 06.
Çѱ¹ÃßÁø °øÇÐȸÁö Á¦ 20±Ç Á¦ 3È£ pp.87-95
ÇÉƲ ±¸µ¿¼Óµµ¿¡ µû¸¥ ÇÉƲ Ã߷±âÀÇ ºñÁ¤»ó»óÅ Ư¼º¿¡ ´ëÇÑ ½ÇÇèÀû ¿¬±¸
Experimental Study on Unsteady-state Characteristics of a Pintle Thruster with Variable Pintle Speeds
ȲÈñ¼º, ÇãȯÀÏ
2016. 03.
Çѱ¹ Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 44±Ç Á¦ 3È£ pp.247-255
¿Áø°ø è¹ö¿ë Æóȸ·Î ¿Á¦¾î½Ã½ºÅÛ ¼³°è ¹× ¼º´ÉÆò°¡
Design and Performance Test of a Closed Loop Thermal Control System for Thermal Vacuum Chamber
¼ÈñÁØ, Á¶ÇõÁø, ¹Ú¼º¿í, ¹®±Í¿ø, Á¤»óÇå, ÇãȯÀÏ
2016. 01
Çѱ¹ Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 44±Ç Á¦ 1È£ pp.88-97
ÃÊ°í¼Ó ºñÇàü Ç׷°¨¼Ò¸¦ À§ÇÑ ¹Ì±¹ÀÇ ºÐ»ç Á¦Æ® ¿¬±¸ µ¿Çâ°ú ÇÙ½É º¯¼ö
Key Parameters and Research Review on Counterflow Jet Study in USA for Drag Reduction of a High-speed Vehicle
±èÁöÈ«, °½Â¿ø, ÀÌÀçû, ÇãȯÀÏ
2016. 01.
Çѱ¹ Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 44±Ç Á¦ 1È£ pp.23-32
ÀÜ¿©ÃßÁøÁ¦ ÃßÁ¤À» À§ÇÑ ¿Áú·®¹ýÀÇ Åë°èÀû ºÒÈ®½Ç¼º ºÐ¼®
Statistical Uncertainty Analysis of Thermal Mass Method for Residual Propellant Estimation
¹ÚÀÀ½Ä, ¹ÚºÀ±Ô, ÇãȯÀÏ
2015. 12.
Çѱ¹ Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 12È£ pp.1116-1123
¿À¸®Çǽº¿¡¼ ±âüÀÇ Ç¥ÁØÀ¯·®À» ÀÌ¿ëÇÑ »ê¼Ò¿Í Çï·ýÀÇ ´©¼³·® ÃøÁ¤¿¡ °üÇÑ ¿¬±¸
Study on Leakage Measurements of Oxygen and Helium Using Standard Gas Flow Rates in a Orifice Flow
ÀÌÁß¿±, ÇÑ»ó¿± , ÇãȯÀÏ
2015. 12.
Çѱ¹ Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 12È£ pp.1108-1115
³ëÁñ ¸ñ ¿ÜºÎÇü ÇÉƲÃ߷±âÀÇ Ãß·ÂƯ¼º¿¡ ´ëÇÑ ¼öÄ¡Çؼ® ¿¬±¸
Numerical Study on Thrust Characteristics of an External Pintle Thruster
ÃÖÁؼ·, ±èµ¿¿¬, ÇãȯÀÏ
2015. 12.
Çѱ¹ Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 12È£ pp.1071-1078
¿Áø°ø è¹ö¿ë ±ØÀú¿Â ºí·Î¿ö ¼³°è ¹× ¼º´ÉÆò°¡
Design and Performance Tests of a Cryogenic Blower for a Thermal Vacuum Chamber
¼ÈñÁØ, Á¶ÇõÁø, ¹Ú¼º¿í, ¹®±Í¿ø, ÇãȯÀÏ
2015. 11.
Çѱ¹ Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 11È£ pp.1008-1015
µ¶ÀÏ DLRÀÇ µà¾ó º§ ³ëÁñ Ư¼º ¹× ÇÙ½É º¯¼ö
Characteristics and Key Parameters of Dual Bell Nozzles of the DLR, Germany
±èÁ¤ÈÆ, ÇãȯÀÏ
2015. 11.
Çѱ¹ Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 11È£ pp.952-962
´ÙÃà ÇÉƲ Ã߷±⿡ Àû¿ëÀ» À§ÇÑ ±¸µ¿ÀåÄ¡ ¿¬µ¿ ¸ÞÄ¿´ÏÁò ¹æ¾È¿¬±¸
Study on Coupling Drive Mechanism for Multi-Axis Pintle Thrusters
ÀÌÀçû, ÇãȯÀÏ, ÀÌÈ£¼º
2015. 08.
Çѱ¹ Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 8È£ pp.722-730
°íµµ º¸Á¤¿ë µà¾ó º§ ³ëÁñ °³¹ß µ¿Çâ°ú ±â¼ú ºÐ¼®
Technology Review and Development Trends of Dual-Bell Nozzle for Altitude Compensation
ÃÖÁؼ·, ÇãȯÀÏ
2015. 05.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 5È£ pp.456~465
1-D ½Ã¹Ä·¹À̼ÇÀ» È°¿ëÇÑ ÇÉƲÃ߷±âÀÇ ¼º´ÉÇؼ® - II : ºñÁ¤»ó»óÅ Ư¼º
Performance Analysis of the Pintle Thruster Using 1-D Simulation - II : Unsteady State Characteristics
³ë¼ºÇö, ±èÁöÈ«, ÇãȯÀÏ
2015. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 4È£ pp.311~317
1-D ½Ã¹Ä·¹À̼ÇÀ» È°¿ëÇÑ ÇÉƲÃ߷±âÀÇ ¼º´ÉÇؼ® - I : Á¤»ó»óÅ Ư¼º
Performance Analysis of the Pintle Thruster Using 1-D Simulation - I : Steady State Characteristics
±èÁöÈ«, ³ë¼ºÇö, ÇãȯÀÏ
2015. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 4È£ pp.304~310
¸óÅ×Ä«¸¦·Î¹æ¹ýÀ» ÀÌ¿ëÇÑ Ãµ¸®¾ÈÀ§¼º ±ËµµÀüÀÌ ¼Ò¿äÃßÁøÁ¦·® ÃßÁ¤¿¡ °üÇÑ ¿¬±¸
COMS GTO Injection Propellant Estimation using Monte-Carlo Method
¹ÚÀÀ½Ä, ÇãȯÀÏ
2015. 01.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 1È£ pp.62~71
Çѱ¹Çü¹ß»çü ¹ß»ç´ë½Ã½ºÅÛ È¿°À¯µµ·Î °³³ä ¼³°è (I)
Conceptual Design of KSLV-II Launch Complex Flame Deflector
¿ÀÈ¿µ, °¼±ÀÏ, ±è´ë·¡, ÀÌÁ¤ÀÏ, ¾öÇü½Ä, ÇãȯÀÏ
2014. 12.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 18±Ç Á¦ 6È£ pp.75~81
Á¤Áö±ËµµÀ§¼ºÀÇ ÀÜ¿©ÃßÁøÁ¦·® ÃøÁ¤¹æ¹ý ¹× ±â¼úµ¿Çâ
Residual Propellant Gauging Methods for Geostationary Satellites and Recent Technology Status
¹ÚÀÀ½Ä, ÇãȯÀÏ
2014. 10.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 42±Ç Á¦ 10È£ pp.870~877
¿ìÁÖ ¿È¯°æ ¸ð»ç¿ë ¼ÒÇü ±ØÀú¿Â ºí·Î¿ö ¼³°è ¹× ¼º´ÉÆò°¡
Design and Performance Test of a Cryogenic Blower for Space Thermal Environment Simulation
¼ÈñÁØ, ¾È¼º¹Î, ÇãȯÀÏ
2013. 10.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 41±Ç Á¦ 10È£ pp.833~839
Áß¾Ó ºÐ»ç ¹æ½Ä ³Ã°¢¼ö ÅõÀÔ¿¡ ÀÇÇÑ ·ÎÄÏ ¿¬¼Ò ÈÄ·ù ³Ã°¢¿¡ °üÇÑ ¿¬±¸
A Study for Rocket Exhaust Flow Cooling due to the Central Spray Type Water Injection
°¼±ÀÏ, ³²Áß¿ø, ÇãȯÀÏ
2013. 07
Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø Ç×°ø¿ìÁÖ±â¼ú Á¦ 12±Ç Á¦ 1È£ pp.163~172
±ËµµÃµÀÌ ¹× ÀÚ¼¼Á¦¾î ½Ã½ºÅÛÀÇ ¿¬±¸°³¹ß µ¿Çâ°ú Àü¸Á
Recent Progress in R&D and Prospect of Divert and Attitude Control System(DACS)
±è¼º¼ö, ÇãȯÀÏ
2012. 12.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 16±Ç Á¦ 6È£ pp.62~72
´ÜÀÏÈÇÐÁ¾ ºñ¹ÝÀÀ Çؼ® ¸ðµ¨À» »ç¿ëÇÑ ·ÎÄÏ ¿¬¼ÒÈÄ·ù À¯µ¿Çؼ® ¿¬±¸
A CFD Study for Rocket Exhaust Flow using Single Species, Unreacted Flow Model
°¼±ÀÏ, ÇãȯÀÏ
2012. 07.
Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø Ç×°ø¿ìÁÖ±â¼ú Á¦ 11±Ç Á¦ 1È£ pp.126~134
Àú±Ëµµ À§¼º °úÇОÀçüÀÇ ¿Çؼ® ¸ðµ¨ °ËÁõÀ» À§ÇÑ ¿¸ðµ¨ º¸Á¤ ¹× È÷ÅÍ ¼³°è
Thermal Model Correlation and Heater Design Verification for LEO Satellite Optical Payload's Thermal Analysis Model Verification
±è¹ÎÀç, ÇãȯÀÏ, ±è»óÈ£, Àå¼ö¿µ, ÀÌ´ö±Ô, À̽ÂÈÆ, ÃÖÇØÁø
2011. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 39±Ç Á¦ 11È£ pp.1069~1076
¾×ü·ÎÄÏ¿£ÁøÀÇ À¯·®Á¶Àý¿¡ °¡º¯¹ëºêÀÇ Á¶Àý±â¹ý°ú Ç÷±Àú Çü»óÀÌ ¹ÌÄ¡´Â ¿µÇâ
Effect of Control Method and Plunger Profile of Variable Valve on Flow Control of a Liquid Rocket Engine
ÀÌÁß¿±, ÇãȯÀÏ
2011. 10.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 15±Ç Á¦ 5È£ pp.35~47
Analysis of formation and breakup mechanisms in rotary atomization through spray visualization
Donghun Lee, Gyungwon You, Seongman Choi, Hwanil Huh
2011. 06.
Journal of visualization
https://doi.org/10.1007/s12650-011-0087-9
Àú±ËµµÀ§¼º ±¤ÇОÀçüÀÇ Áö»ó ¿Áø°ø ½ÃÇèÀ» À§ÇÑ ¿¹ºñ ¿Çؼ®
Preliminary Thermal Analysis for LEO Satellite Optical Payload's Thermal Vacuum Test
ÀÌÁ¾·ü, ÇãȯÀÏ, ±è»óÈ£, Àå¼ö¿µ, ÀÌ´ö±Ô, À̽ÂÈÆ, ÃÖÇØÁø
2011. 05.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 39±Ç 5È£ pp.466~473
¸¶ÀÌÅ©·Î µ¿·Â¹ß»ý¿ë ¼ÒÇü ½ºÀ§½º·Ñ ¿¬¼Ò±âÀÇ Å©±â¿Í Çü»ó È¿°ú¿¡ ´ëÇÑ ¿¬±¸
Effect of Scale and Geometry on the Performance of Heat-Recirculating Swiss roll combustors for Micro Power Generation Applications
¿ÀÈ¿µ, ÇãȯÀÏ, Paul D. Ronney
2011. 02.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 15±Ç 1È£ pp.1~10
ÇÏÀ̺긮µå ·ÎÄÏÀÇ Ãß·ÂÁ¦¾î ¼º´É Çâ»ó¿¡ °üÇÑ ¿¬±¸
Study of Thrust Control Performance Improvement for Hybrid Rocket Applications
ÃÖÀ缺, °¿Ï±Ô, ÇãȯÀÏ
2011. 02.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 15±Ç 1È£ pp.55~62
¿¬·áÀüÁö °³Áú±â·Î È°¿ëÀ» À§ÇÑ ½ºÀ§½º ·Ñ ¿¬¼Ò±âÀÇ Å©±â¿Í ¿¬·áÀÇ Á¾·ù¿¡ µû¸¥ Ư¼º¿¬±¸
Effect of Scale and Fuel Type on Heat-recirculating Swiss-roll Combustor Performance for Fuel Cell Reformer Applications
±è¿¬È£, ÇãȯÀÏ, Paul D. Ronney
2011. 12.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 14±Ç 6È£ pp.11~18
Çѱ¹°úÇбâ¼ú´ÜüÃÑ¿¬ÇÕȸ - °úÇбâ¼ú¿ì¼ö³í¹®»ó ¼ö»ó! (2011³â 7¿ù 5ÀÏ)
Àü±âÃßÁø 1Åæ±Þ Personal Air VehicleÀÇ µ¿·Â½Ã½ºÅÛ ¿¹ºñ ºÐ¼®
Preliminary Analysis of Power Systems for 1-ton class Electric Powered PAV
À±µ¿ÀÍ, ÇãȯÀÏ, ¾ç¼ö¼®
2010. 12.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 14±Ç 6È£ pp.1~8
°¡½º¹ß»ý±â ¿¬·á°³Æó¹ëºêÀÇ µ¿Àû °Åµ¿
Dynamic Characteristics for Fuel Shutoff Valve of a Gas Generator
ÀÌÁß¿±, ÇãȯÀÏ
2010. 08.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 14±Ç 4È£ pp.1~9
UAV ÃßÁø±â°üÀÇ Á¾·ù ¹× Ư¼º¿¡ °üÇÑ ±â¼úÀû °íÂû
Technical Survey on the Classification and Characteristics of UAV's Power Plants
À̵¿ÈÆ, Æر⼮, ±èÀ¯ÀÏ, ¹ÚºÎ¹Î, ÃÖ¼º¸¸, ÇãȯÀÏ
2010. 06.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 14±Ç 3È£ pp.79~86
ÀΰøÀ§¼º žÀçÇ° ¼öÁØ ¿Áø°ø ½ÃÇè¿¡ ´ëÇÑ ¿Çؼ® ¸ðµ¨ÀÇ °³¹ß°ú ȯ°æ½ÃÇè °á°ú¸¦ ÀÌ¿ëÇÑ °ËÁõ
Development and verification of Thermal Analysis Model for Thermal vacuum Test of Satellite Components
±è»óÈ£, ¼Çö¼®, À¯ÀçÈ£, ÇÑÀº¼ö, ±èÅ°æ, ±èÇüµ¿, ÇãȯÀÏ
2010. 08.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 38±Ç 8È£ pp.842~847
GO 2 /PE ÇÏÀ̺긮µå ·ÎÄÏÀÇ Ãß·ÂÁ¦¾î¸¦ À§ÇÑ ½Ã½ºÅÛ ¼³°è ¹× ±âÃʽÇÇè
Sytem Design and Fundamental Experiment for Thrust Control of GO2/PE Hybrid Rocket
ÀÌ¿ë¿ì, °¿Ï±Ô, ÇãȯÀÏ
2010. 02.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 14±Ç 1È£ pp.40~47
°¡½º¹ß»ý±â »êÈÁ¦ °³Æó¹ëºêÀÇ ³»ºÎ À¯µ¿Æ¯¼º ¹× ±¸Á¶Çؼ®¿¡ °üÇÑ ¿¬±¸
Study on Flow Property and Structural Analysis of Gas Generator Oxidant On/Off valve
ÀÌÁ¾·ü, ÇãȯÀÏ, ¾È¾ç¿ì
2009. 12.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 13±Ç 6È£ pp.48~55
Personal Air VehicleÀÇ ÃßÁø½Ã½ºÅÛ¿¡ ´ëÇÑ ±â¼úÀû °íÂû
Thchnical Survey on Propulsion Systems for Personal Air Vehicles
À±µ¿ÀÍ, ÇãȯÀÏ
2009. 12.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 13±Ç 6È£ pp.56~63
µå·³Çü ȸÀü¿¬·á³ëÁñÀÇ ¹Ì¸³È ±â±¸ ¹× ºÐ¹«Æ¯¼º ¿¬±¸
The Atomization Mechanism and Spray Characteristics of Drum Type Rotary Atomizer
À̵¿ÈÆ, ÃÖÇö°æ, ÃÖ¼º¸¸, À¯°æ¿ø, ÇãȯÀÏ
2008. 04.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 12±Ç 2È£ pp.57~65
¸¶ÀÌÅ©·Î ÃßÁøÀåÄ¡¿¡ Àû¿ëÀ» À§ÇÑ ´©¼¾¼ö¿¡ µû¸¥ ¿Àû¹ß»ê¿ø¸®ÀÇ È¿À²ºÐ¼®
Efficiency Analysis of Thermal Transpiration According to Knudsen Number for Application to Micro-propulsion System
Á¤¼ºÃ¶, ÇãȯÀÏ
2008. 05.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 36±Ç 5È£ pp.483~490
¼¼Â÷Á¦Æ®³ëÁñ ¿¬¼Ò±âÀÇ À¯µ¿Æ¯¼º
Fludic Characteristics of Precessing Jet Nozzle Combustor
ÀÌÇý¿µ, ÇãȯÀÏ
2007. 08.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 11±Ç 4È£ pp.1~9
ÃʼÒÇü ³ëÁñ À¯µ¿Àå¿¡ °üÇÑ ¼öÄ¡Àû ¿¬±¸
A Computational Study on the Characteristics of Flowfields in micro Nozzles
¼ÁöÇÑ, Á¶Çö±¸, À̵¿È£, Á¤¼ºÃ¶, ¸í³ë½Å, ÇãȯÀÏ
2007. 12.
Çѱ¹Àü»êÀ¯Ã¼°øÇÐȸÁö Á¦ 12±Ç 4È£ pp.38~43
³Ã°¡½º ÃßÁøÀåÄ¡¸¦ ÀÌ¿ëÇÑ ¸¶ÀÌÅ©·Î ³ëÁñÀÇ ¼º´ÉÆò°¡
Performance Evaluation of Micro-nozzle Using cold Gas Propulsion System
Á¤¼ºÃ¶, ±è¿¬È£, ¿ÀÈ¿µ, ÇãȯÀÏ, ¸í³ë½Å
2007. 12.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 11±Ç 6È£ pp.42~49
¾×ü ·ÎÄÏ¿£Áø¿¡¼ ¼±Çü ¿¬¼Ò ¾ÈÁ¤ÇÑ°è¿¡ ¹ÌÄ¡´Â À¯ÇÑÈÇйÝÀÀ ¹× ¸·³Ã°¢ È¿°ú
Effects of Finite-Rate Chemistry and Film Cooling on Linear Combustion-Stability limit in Liquid rocket Engines
¼ÕäÈÆ, ¹ÚÀ̼±, ¹®À±¿Ï, ±èÈ«Áý, ÇãȯÀÏ
2006. 02.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 34±Ç 2È£ pp.75~81
¸¶ÀÌÅ©·Î ³ëÁñ ¼º´É Æò°¡
Performance test of micronozzle
¹®¼ºÈ¯, ¿ÀÈ¿µ, ÇãȯÀÏ
2005. 05.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 33±Ç 5È£ pp.72~78
LPG ¾×»óºÐ»ç ¿£Áø¿¡¼ ¾Æ¼¼Åæ PLIF¸¦ ÀÌ¿ëÇÑ ¿¬·áºÐÆ÷ ÃøÁ¤±â¹ý ¿¬±¸
Acetone PLIF for Fuel Distribution measurements in Liquid Phase LPG Injection Engine
¹Ú½ÂÀç, ÇãȯÀÏ, ¿À½Â¹¬, °°Ç¿ë, ¹èÃæ½Ä
2004. 01.
Çѱ¹ÀÚµ¿Â÷°øÇÐȸ Á¦ 12±Ç 1È£ pp.74~82
¸¶ÀÌÅ©·Î ÄÝµå °¡½º Ã߷±âÀÇ ¼±Çà ¿¬±¸
Preliminary Study of Micro Cold Gas Thruster
¹®¼ºÈ¯, ¿ÀÈ¿µ, ÇãȯÀÏ
2004. 04.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 8±Ç 2È£ pp.54~61
¼ÒÇü ¾×ü ÃßÁø±â°ü ¿¬¼Ò ½ÃÇèÀ» À§ÇÑ Ãß·Â ÃøÁ¤ ÀåÄ¡ÀÇ ¼º´É Ư¼º ¿¬±¸
Perfomance Characteristics of Thrust measurement System for Hot-Firing Test of small Liquid Propulsion Engines
±èÀÎÅÂ, ÇãȯÀÏ, ±èÁ¤¼ö, Àå±â¿ø, ÀÌÀç¿ø
2004. 09.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 32±Ç 9È£ pp.122~129
¾×ü ·ÎÄÏ¿£ÁøÀÇ ¿¬¼Ò ºÒ¾ÈÁ¤¼º ¿¬±¸ µ¿Çâ
Combustion Instability of Liquid Rocket Engines
¼º´ëÇö, ÇãȯÀÏ, ¼ÕÀçÈÆ
2004. 09.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 32±Ç 9È£ pp.153~161
¾×ü ·ÎÄÏ¿£Áø¿¡¼ ¼±Çü ¿¬¼Ò ºÒ¾ÈÁ¤ Çؼ®À» ÀÌ¿ëÇÑ ¿¬¼Ò ¾ÈÁ¤ÇÑ°è °î¼± °è»ê
Calculation of Comnustion Stability Limits Using Linear Stability Analysis in Liquid Rocket Engines
¼ÕäÈÆ, ¹®À±¿Ï, ÇãȯÀÏ
2004. 10.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 32±Ç 10È£ pp.93~101
Àú±Ëµµ À§¼ºÀÇ ÃßÁøÁ¦ ¼Ò¸ðÀ² °èÃø¿¡ °üÇÑ °íÂû
An investigation on the Propellant Comsumption Rate gauged from the low-Earth-orbit Spacecraft
±èÀÎÅÂ, ÇãȯÀÏ, ±èÁ¤¼ö
2003. 01.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 31±Ç Á¦ 1È£ pp.113~119
ÃÊÀ½¼Ó ¿¬¼Ò±â ³»ºÎÀÇ Ãß·Â ºÐÆ÷ °è»êÃÊÀ½¼Ó ¿¬¼Ò±â ³»ºÎÀÇ Ãß·Â ºÐÆ÷ °è»ê
Determination of Thrust Distribution in the Supersonic Combustor
ÇãȯÀÏ
2003. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 31±Ç Á¦ 4È£ pp.69~75
ÃÊÀ½¼Ó dzµ¿ÀÇ Ãß·Â ÃøÁ¤ ¹æ¹ý ºñ±³
Comparison of thrust measurement of a supersonic Wind Tunnel
±èÇü¹Î, ÇãȯÀÏ
2003. 05.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 31±Ç Á¦ 5È£ pp.93~99
±ØÃÊÀ½¼Ó ÃßÁø±â°ü ¿¬±¸¸¦ À§ÇÑ 2Â÷¿ø ÃÊÀ½¼Ó dzµ¿ ¼³°è ¹× Á¦ÀÛ
Development of a 2-D Supersonic Wind Tunnel for Hypersonic Propulsion Study
±èÁ¤¿ë, ±èÇü¹Î, ÇãȯÀÏ
2003.
»ê¾÷±â¼ú¿¬±¸¼Ò ³í¹®Áý Á¦ 18±Ç Á¦ 1È£ pp.49~56
Numerical study of Mixing Enhancement Shock Waves in Model Scramjet Engine
Jiho Kim, Youngbin Yoon, Hwanil Huh, Jeonyeol Choi
2003. 06.
AIAA Journal Vol.41 No.6 pp.1074~1080
https://doi.org/10.2514/2.2047
¾×ü·ÎÄÏ¿£Áø °íÁÖÆÄ ¿¬¼ÒºÒ¾ÈÁ¤ÀÇ ¿¹Ãø
Prediction of High Frequency Combustion Instabilities of a Liquid Rocket Engine
À±¿õ¼·, ÇãȯÀÏ
2003. 06.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 7±Ç 3È£ pp.61~68
¿ìÁÖºñÇàü ÃßÁø½Ã½ºÅÛ ÈÇÐ½Ä Ã߷±âÀÇ °³¹ß ÇöȲ
Development Status of Chemical Thruster Equipped on Space Vehicle Propulsion System
±èÁ¤¼ö, ±èÀÎÅÂ, ÇãȯÀÏ
2003. 08.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 7±Ç 4È£ pp.80~89
Application of Low NOx Combustion Method to Regenerative Oxygen Enriched Combustor
Huh, H(ÇãȯÀÏ), Seo, J.W.(¼Á¤¿ø), Noh, D.S.(³ëµ¿¼ø)
2002. 06.
Twenty-Ninth International Symposium on Combustion
Two Color PIV ±â¹ýÀ» ÀÌ¿ëÇÑ ·¥Á¦Æ®¿£Áø ¿¬¼Ò±â Ư¼º¿¡ ´ëÇÑ ¿¬±¸
A Study on the Characteristics of the Ramjet Engine Combustor using a Two color PIV Technique
¾È±Ôº¹, À±¿µºó, Á¤Àμ®, ÇãȯÀÏ
2002. 01.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 30±Ç 1È£ pp.95~104
ÇÏÀ̺긮µå ·ÎÄÏÀÇ °³³ä ¼Ò°³ ¹× ¿¬±¸°³¹ß µ¿Ç⠺м® ¥± - ´ëÇÐ ¹× ¾Æ¸¶Ãß¾î
Recent Progress in Research and Development of Hybrid Rocket:PART ¥±. Research activities of University and Amateurs
±Ç¹ÎÂù, ÇãȯÀÏ
2002. 03.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 30±Ç 3È£ pp.155~163
ÇÏÀ̺긮µå ·ÎÄÏÀÇ °³³ä ¼Ò°³ ¹× ¿¬±¸°³¹ß µ¿Ç⠺м® ¥° - ´ëÇü ÇÁ·ÎÁ§Æ® ¹× ±â¾÷À» Áß½ÉÀ¸·Î
Recent Progress in Research and Development of Hybrid Rocket:PART ¥° International Development Programs of Hybrid Rocket
±Ç¹ÎÂù, Çã`1ȯÀÏ
2002. 03.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 30±Ç 3È£ pp.146~154
¿¡¸ÖÁ¯ ¿¬·á¸¦ ÀÌ¿ëÇÑ µðÁ©¿£ÁøÀÇ ºÐ¹« ¹× ¹è±âƯ¼º ¿¬±¸
Spray Characteristics and Exhaust Emission Tests for a Diesel Engine Using Emulsified Fuels
¼ÈñÁØ, ¿À½Â¹¬, ÇãȯÀÏ
2002. 04.
Çѱ¹ÀÚµ¿Â÷°øÇÐȸ ³í¹®Áý Á¦ 10±Ç 4È£ pp.61~68
Combustion Efficiencies of Supersonic Flames
Albert Ratner, James F. Driscoll, Hwanil Huh, Rodney A
2001. 03.
Journal of Propulsion and Power Vol. 17 No.2 pp.301~307
https://doi.org/10.2514/2.5742
¸¶ÀÌÅ©·Î ÃßÁøÀåÄ¡
Micro Propulsion System
ÀüÀ翵, À±¿µºó, ÇãȯÀÏ
2001. 06.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 5±Ç 3È£ pp.100~107
¸ðµ¨ ½ºÅ©·½Á¦Æ® ¿£Áø³»ÀÇ Ãæ°ÝÆÄ À¯µµ È¥ÇÕ Áõ´ë¿¡ °üÇÑ ¿¬±¸
Numerical Study on Mixing Enhancement by Shock Waves in a Model SCRamjet Engine
±èÁöÈ£, ÇãȯÀÏ, ÃÖÁ¤¿, À±Çüºó, Á¤Àμ®
2000. 01.
Ç×°ø¿ìÁֽűâ¼ú¿¬±¸¼Ò ¿¬±¸º¹°í Á¦ 1±Ç 1È£ pp.30~46
Ãæ°ÝÆÄ°¡ ÃÊÀ½¼Ó ¼ö¼Ò-°ø±â È¿°ÀÇ ¾ÈÁ¤ÇÑ°è¿¡ ¹ÌÄ¡´Â ¿µÇâ
Measured Effect of Shock Wave on the Stability Limits of Supersonic hydrogen-Air Flames
ÇãȯÀÏ
1999. 02.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 3±Ç 1È£ pp.86~94
¸ðµ¨ ½ºÅ©·¥Á¦Æ® ¿¬¼Ò±â¿¡¼ Ãæ°ÝÆÄ ¿µÇâ¿¡ ´ëÇÑ ½ÇÇèÀû ¿¬±¸
An Experimental Study of Shock Wave Effects on the Model SCRamjet Combustor
ÇãȯÀÏ
1999. 02.
Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 3±Ç 1È£ pp.65~71
¸ðµ¨ ½ºÅ©·¥Á¦Æ® ¿¬¼Ò±â¿¡¼ÀÇ ÃÊÀ½¼Ó ¼ö¼Ò-°ø±â Á¦Æ® È¿°¿¡ ´ëÇÑ Ãæ°ÝÆÄÀÇ ¿µÇâ
Effects of Shock Waves on a Supersonic Hydrogen-Air Jet Flame in a Model SCRamjet Combustor
±èÁöÈ£, ÇãȯÀÏ, ÃÖÁ¤¿, À±Çüºó, Á¤Àμ®
1999. 03.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 27±Ç 3È£ pp.110~118
Measured Supersonic Flame Properties: Heat-Release Patterns, Pressure Losses, Thermal Choking Limits
Yoon, Y., Donbar, U.M., Huh, H., Droscoll, J.F.
1996. 01.
AIAA, Journal of Propulsion and Power, 12, pp. 718~723
https://doi.org/10.2514/3.24093