ScholarWorks@Hanyang University: Cho, Jin Soo

Detailed Information

Cho, Jin Soo (조진수)

서울 공과대학 (서울 기계공학부)

Research Area

Tel
Homepage

ResearcherID ORCiD Scopus Google Scholar ID ResearchGate

Keyword

Boundary Element Method(경계요소법):8||Flaperon(플래퍼론):5||UV lamps:4||Computational Fluid Dynamics:4||Gas Turbine:4||Wing In Ground Effect(지면효과):4||WingInGround Effect(지면효과):4||Counterrotating vortex:3||Discharge coefficient:3||Preswirler:3||Secondary Air System:3||Aerodynamic analysis:3||Discharge Coefficient:3||Optimization:3||UV reactor:3||Wind Tunnel Testing(풍동시험):2||boundary element method:2||Inlet shape:2||Iterative Decambering Approach:2||Iterative Decambering Approach(반복적 캠버변형 기법):2||AirPressureLevitated HighSpeed Ground Vehicle(공압부양 고속 지상운송체):2||fluence rate:2||BWB(Blended Wing Body:2||Lateral Spacing(가로간격):2||Formation Flight(편대 비행):2||Relative Navigation (상대 항법):2||Line Formation(일렬편대):2||Longitudinal Stability(종방향 안정성):2||MAV Propeller(초소형 무인기 프로펠러):2||Sduct:2||MAV(Micro Air Vehicle:2||CFD analysis:2||Secondary air system:2||Adiabatic effectiveness:2||Frequency Domain Panel Method(주파수영역 패널법):2||Newton Iteration:2||Stability and Control(조종 안정성):2||Stall Prediction:2||water disinfection:2||wing in ground effect:2||Steady(정상상태):2||Newton Iteration(뉴턴 반복법):2||Sudden accelation(급가속):2||Distortion coefficient:2||Nonlinear Aerodynamic Characteristics(비선형 공력특성):2||Nonplanar Ground Surface(비평면 지면):2||Tandem Wing(종렬날개):2||뉴턴 반복법:2||반복적 캠버변형 기법:2||Tandem Wing(탠덤 날개):2||비평면 양력면 이론:2||Nonplanar Lifting Surface Theory:2||Nonplanar Surface(비평면):2||Frequencydomain Panel Method(주파수 영역 패널법):2||실속 예측:2||Future Air Speed Transit(차세대 초고속 운송시스템):2||융합익기):2||Time Stepping Method(시간전진법):2||GPS:2||전산유체역학:2||Timedomain panel method(시간영역 패널법):2||초소형 비행체):2||Tip Clearance:2||Aerodynamic Design(공력설계):2||Gas turbine:2||Channel(수로형 안내로):2||Aerodynamic loss:2||Particle Filter (파티클 필터):2||Pitch oscillation(피치진동):2||Helicopter rotor:2||Unsteady Aerodynamic Analysis(비정상 공력해석):2||High Speed Ground Transporter(고속 운송체):2||Unsteady(비정상):2||Vee Formation(V자편대) Lift Drag Ratio(양항비):2||Vision Sensor (비전 센서):2||Vortex Lattice Method(와류격자법):2||Boundary layer thickness:2||BoundaryElement Method(경계요소법):2||Wind Tunnel Test:2||Wind Tunnel Test(풍동 시험):2||MOGA:1||Matrix method:1||Multidisciplinary design optimization:1||Nearwall Treatment Methods:1||Newton iteration:1||Numerical simulation:1||Offdesign:1||Optimal LatinHypercube Design(OLHD):1||Optimization Process:1||Optimization(최적화):1||Panel method:1||Panel method(패널법):1||Parametric study:1||Perforated Plate:1||Pitchbreak:1||Preswirl Nozzle:1||Preswirl System:1||Preswirl nozzle:1||Preswirl system:1||Preswirler(프리스월러):1||Pressure Loss:1||Pressure Loss Coefficient:1||Pressure Recovery:1||RED:1||Radial OnBoard Injection Type Preswirl System:1||Radial OnBoard Injection(반경 방향 분사 방식):1||Radiation modeling:1||Receiver Hole:1||Receiver hole:1||Relative roughness:1||Response surface:1||Reynolds number:1||SDuct:1||Sshaped intake:1||Scavenger radicals:1||Secondary air system(이차 유로 시스템):1||Serrated Trailing Edge:1||Sirocco fan(시로코 팬):1||Splitter:1||Sub Duct:1||Surface roughness:1||Swirl Ratio:1||Swirl ratio:1||Tangential OnBoard Injection(접선 방향 분사 방식):1||Temperature Drop Efficiency:1||Temperature drop:1||Temperature drop effectiveness(온도강하 효율):1||TimeDomain panel methed:1||Timestepping method(시간전진법):1||Tip Leakage Flow:1||Total Pressure Loss Coefficient:1||Turbine Load:1||U80 propeller:1||UAV(무인 항공기):1||UAV(무인항공기):1||UCAV:1||UV disinfection:1||Uniform flow index:1||Unsteady Panel Method:1||Wake Rollup:1||Water disinfection:1||Wind tunnel testing:1||Wing twist:1||biomimetics:1||channeltype guideway:1||computational fluid dynamics:1||discharge coefficient:1||fish swimming:1||fishlike foils:1||frequencydomain panel method:1||friction coefficient:1||genetic algorithms:1||geometry defeaturing:1||high speed ground transporter:1||iterative decambering approach:1||kernel function:1||lifting surface method:1||micro air vehicle:1||micro air vehicle propeller design:1||multiple bank operation:1||nonlinear aerodynamic characteristics:1||nonplanar surface:1||openchanneltype UV reactor:1||preswirl system:1||rail:1||reduction equivalent dose:1||secondary air system:1||unsteady panel method:1||vane type nozzle:1||가스 터빈:1||격자볼츠만 법:1||공력소음:1||광역소음:1||날개 끝 누설 와류:1||날개 통과 주파수:1||냉각 시스템:1||비정상 패널법:1||생체 모방익:1||생체 형상가변익:1||스월비:1||유량계수:1||이산소음:1||이중구조팬:1||전압력손실계수:1||진화 알고리즘:1||최적화 과정:1||톱니형 뒷전:1||프리스월러:1||":1||후류 말림:1||(Broadband noise):1||AOP reactor:1||Active flow control:1||Aeroacoustics (Discrete noise):1||Aerodynamic Characteristics:1||Aerodynamic analysis(공력해석):1||Aerodynamic characteristics:1||Air purifier(공기청정기):1||Ambient Air Temperature:1||Angle of incidence:1||Aspect ratio:1||Avionic Equipment(항공기용 전자 장비):1||Axial clearance:1||BWB(융합익기):1||Batwing":1||Biomorphing Foil:1||Blade Passing Frequency (BPF):1||Blade tip cavity:1||Blendedwingbody:1||Blockage effect(봉쇄 효과):1||Boundary Layer Suction:1||Boundary layer suction:1||Business jet:1||CFD:1||CFD Analysis:1||CFD(전산유체역학):1||Centrifugal compressor:1||Chamfer:1||Colebrook equation:1||Computational Fluid Dynamics(전산유체역학):1||Computational Fluids Dynamics:1||Computational fluid dynamics:1||Computational fluid dynamics(전산 유체 역학):1||Computational fluid dynamics(전산유체역학):1||Conic Winglet:1||Conjugate Heat Transfer:1||Conjugate heat transfer:1||Cooled Turbine:1||Cooling Path:1||Cooling Performance Analysis(방열 성능 해석):1||Cooling System:1||Cooling System(냉각 시스템):1||Cooling effectiveness:1||CounterRotating Ducted Fan:1||Crosswind:1||Design of the Heat Sink (히트싱크 설계):1||Discharge coefficient(유량계수):1||Disk friction loss:1||Distortion cefficient:1||Dual Fan:1||Ducted Fan:1||Ducted fan:1||Evolution Algorithm:1||FaninWing(팬인윙):1||Film Cooling Effectiveness:1||Flow Distortion:1||Flow Separation:1||Flow characteristics:1||Flow distortion:1||Fluence rate:1||Forward flight:1||Forwardcurved(전향익):1||Free vortex design:1||Free wake:1||Frequency domain panel method:1||Gas Turbine Vane:1||Gas Turbine(가스 터빈):1||Geometry Effect:1||Heat transfer coefficient:1||High pressure cooled turbine:1||Hover:1||Hybrid Electricpropulsion System(하이브리드 전기추진시스템):1||Impeller disk plane:1||Key Words :Biomimetic Foil:1||Kriging:1||Lambda wing configuration:1||LatticeBoltzman Method:1||Lift fan(양력 팬):1||MAV:1||

STATISTICS: Total View :4,979,302; Today View :351

RSS_1.0 RSS_2.0 ATOM_1.0

222, Wangsimni-ro, Seongdong-gu, Seoul, 04763, Korea+82-2-2220-1365

Certain data included herein are derived from the © Web of Science of Clarivate Analytics. All rights reserved.
You may not copy or re-distribute this material in whole or in part without the prior written consent of Clarivate Analytics.

Detailed Information

Keyword

BROWSE