우수 논문은 메릭인인터뷰를 통해 추천된 저자의 논문자료를 재분류한 콘텐츠입니다.
논문의 가치 평가는 논문의 내용과 학술지와 인용 수 등의 자료들을 참조해 주세요.
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Flow Characteristics of Three-Dimensional Curved Wall Jets on a Cylinder
Cited by 19
Mirae Kim
(Pusan National University)
Journal of Fluids Engineering
2018
Flow separation, Nozzles, Momentum, Shear stress
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Transient three-dimensional flow structures of oblique jet impingement on a circ...
Cited by 14
Mirae Kim
(Pusan National University)
Journal of Visualization
2018
Impinging jet, 3D flow structure, Cylinder,
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Flow and surface pressure field measurements on a circular cylinder with impinge...
Cited by 6
Mirae Kim
(Pusan National University)
Experimental Thermal and Fluid Science
2019
Turbulent round jet, Impingement, 3D curved wall jet, Stereo PIV, Pressure sensitive paint
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Experimental study on heat transfer and flow structures of feedback-free sweepin...
Cited by 12
MiraeKim
(Pusan National University)
International Journal of Heat and Mass Transfer
2020
Time-resolved particle image velocimetry, Surface heat transfer
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Measurement of three-dimensional flow structure and transient heat transfer on c...
Cited by 5
MiraeKim
(Pusan National University)
International Journal of Heat and Mass Transfer
2020
Impinging jet, Curved surface, Transient heat transfer
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Polynomial Guidance Laws Considering Terminal Impact Angle and Acceleration Cons...
Cited by 141
Chang-Hun Lee
(KAIST)
IEEE Transactions on Aerospace and Electronic Syst
2013
Acceleration, Missiles, Polynomials, Trajectory, Kinematics, Gravity
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Generalized Formulation of Weighted Optimal Guidance Laws with Impact Angle Cons...
Cited by 71
Chang-Hun Lee
(KAIST)
IEEE Transactions on Aerospace and Electronic Syst
2013
Acceleration, Cost function, Optimal control, Missiles, Kinematics, Equations
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Connections Between Linear and Nonlinear Missile Autopilots via Three-Loop Topol...
Cited by 23
Chang-Hun Lee
(Agency for Defense Development)
Journal of Guidance, Control, and Dynamics
2016
via Three-Loop Topology
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Optimality of Error Dynamics in Missile Guidance Problems
Cited by 50
Shaoming He
(Cranfield University)
Journal of Guidance, Control, and Dynamics
2018
Missile Guidance Problems
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Convex Optimization-based Entry Guidance for Spaceplane
Cited by
Juho Bae
(KAIST)
International Journal of Control, Automation and S
2022
Spaceplane
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