본문 바로 가기

국내 최대 기계 및 로봇 연구정보

메릭人

우수 논문

우수 논문은 메릭인인터뷰를 통해 추천된 저자의 논문자료를 재분류한 콘텐츠입니다.
논문의 가치 평가는 논문의 내용과 학술지와 인용 수 등의 자료들을 참조해 주세요.

논문분석 리스트
	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
	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,
	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
	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
	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
	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
	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
	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
	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
	Convex Optimization-based Entry Guidance for Spaceplane \| Cited by Juho Bae (KAIST) International Journal of Control, Automation and S \|2022 Spaceplane

앞으로

처음으로 1 2 3 4 5 6 7 8 9 10

앞으로

서브 우측상단1

주소 : 부산광역시 금정구 장전 2동 부산대학교 제 11 공학관 407호 기계·로봇 연구정보센터

E-mail: ariass@naver.com Tel : 051-510-1384~5(전화 전에 클릭) Fax : 051-516-2029

Copyright (c) 2021 MERRIC. All Rights Reserved.

굿 콘텐츠 인증마크