Zobrazeno 1 - 10 of 26 pro vyhledávání: '"Seonghee Kho"'
1
Akademický článek
Structural Stability Analysis of Underwater High-Speed Moving Vehicles in Supercavity Flow Velocity
Autor: Kyungwon Oh, Seonghee Kho
Publikováno v: Aerospace, Vol 10, Iss 11, p 916 (2023)
The purpose of this paper is to analyze the structural stability of an underwater high-speed vehicle. The drag characteristics of a moving body moving at high speed in water were analyzed, and a stability analysis of the structure was performed by ap
Externí odkaz: https://doaj.org/article/dd1d3d96cc5243b3a62b5c31223fdc5b
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2
Akademický článek
Design of the Electronic Engine Control Unit Performance Test System of Aircraft
Autor: Seonghee Kho, Hyunbum Park
Publikováno v: Aerospace, Vol 8, Iss 6, p 158 (2021)
In this study, a real-time engine model and a test bench were developed to verify the performance of the EECU (electronic engine control unit) of a turbofan engine. The target engine is a DGEN 380 developed by the Price Induction company. The functio
Externí odkaz: https://doaj.org/article/d41d52633fcd45d9bbda3b3b98cdec11
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4
Design of the Electronic Engine Control Unit Performance Test System of Aircraft
Autor: Hyunbum Park, Seonghee Kho
Publikováno v: Aerospace
Volume 8
Issue 6
Aerospace, Vol 8, Iss 158, p 158 (2021)
In this study, a real-time engine model and a test bench were developed to verify the performance of the EECU (electronic engine control unit) of a turbofan engine. The target engine is a DGEN 380 developed by the Price Induction company. The functio
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fc6d061bad27d855b16a14ddc14d3d24
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6
Development of Practical Integral Condition Monitoring System for A Small Turbojet Engine Using SIMULINK and LabVIEW
Autor: Seonghee Kho, Changduk Kong, Gwanglim Park, Gilsu Park
Publikováno v: Journal of the Korean Society of Propulsion Engineers. 17:80-88
In currently developed engine condition monitoring systems, most field engine maintenance engineers have difficulties to use them in fields due to complexity, unpractical use, lack of understanding, etc. Therefore a practical usable engine condition
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::253486b7d9a4fc95c9f9c2bf99731919
https://doi.org/10.6108/kspe.2013.17.1.080
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7
Study of On-line Performance Diagnostic Program of A Helicopter Turboshaft Engine
Autor: Hyeok Ryu, Seonghee Kho, Changduk Kong, Youngju Koo
Publikováno v: Journal of the Korean Society for Aeronautical & Space Sciences. 37:1238-1244
5IJT XPSL QSPQPTFT B (6* UZQF PO MJOF EJBHOPTUJD QSPHSBN VTJOH 4*.6-*/, BOE'V[[Z /FVSP BMHPSJUINT GPS B IF MJDPQUFS UVSCPTIBGU FOHJOF %VSJ OH EFWFMPQNFOU PG UIFEJBHOPTUJDQSPHSBNBMPPL VQUBCMFUZQFCBTFQFSGPSNBODFNPEVMF GPS SFEVDJOHDPNQVUFS DBMDVMBUJOH U
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::fb9518da2ddf23c48e6a6a00f9490a5b
https://doi.org/10.5139/jksas.2009.37.12.1238
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8
Development of On-line Performance Diagnostic Program of a Helicopter Turboshaft Engine
Autor: Seonghee Kho, Changduk Kong, Hyeok Ryu, Youngju Koo
Publikováno v: International Journal of Aeronautical and Space Sciences. 10:34-42
Gas turbine performance diagnostics is a method for detecting, isolating and quantifying faults in gas turbine gas path components. On-line precise fault diagnosis can promote greatly reliability and availability of gas turbine in real time operation
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::8b624a297d8f10c42d60774303173ef5
https://doi.org/10.5139/ijass.2009.10.2.034
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9
A Study on Multi-Fault Diagnosis for Turboshaft Engine of UAV Using Fuzzy and Neural Networks
Autor: Seonghee Kho, Changduk Kong, Changho Lee, Jayoung Ki, Youngju Koo
Publikováno v: Journal of the Korean Society for Aeronautical Space Science. 37:556-561
The UAV(Unmanned Aerial Vehicle) that is remotely operating in various and long flight environments must have a very reliable propulsion system. Precise fault diagnosis of the turbo shaft engine for the Smart UAV that has the vertical take-off, landi
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::c4620d0cae3fbe563decfcf5042e6e5b
https://doi.org/10.5139/jksas.2009.37.6.556
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10
Improvement on Performance Simulation Using Component Maps of Aircraft Gas Turbine Obtained from System Identification
Autor: Seonghee Kho, Changduk Kong, Jayoung Ki
Publikováno v: Journal of the Korean Society for Aeronautical & Space Sciences. 32:96-103
Sought a set of component performance lines from experiment data or some data supplied in the engine manufacturer to improve the traditional scaling method and suggested a map scaling method that construct component performance lines newly using poly
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::73f555fc3909abbf5f20ee35c853fff7
https://doi.org/10.5139/jksas.2004.32.6.096
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