Waseda University · Engineering
켄지 다키자와 교수의 연구실은 유체-구조 상호작용(FSI) 및 열유체 해석을 중심으로 한 고정밀 수치 시뮬레이션 기법을 개발하고 있습니다. 특히, 움직임과 변형이 있는 경계를 가진 유동 문제를 위한 특수한 공간-시간 스킴, 다중스케일 기법, 슬립 인터페이스 처리 기술 등을 통해 항공우주, 자동차, 심장혈관 등 다양한 분야의 복잡한 유체역학 문제를 정밀하게 해석합니다. 연구는 환자 맞춤형 심장혈관 모델링에서부터 차량 및 로켓 편의성 향상을 위한 고도화된 수치 기법까지 응용 범위가 넓습니다.
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We present the special space-time computational techniques we have introduced recently for computation of flow problems with moving and deforming solid surfaces. The techniques have been designed in the context of the deforming-spatial-domain/stabilized space-time formulation, which was developed by the Team for Advanced Flow Simulation and Modeling for computation of flow problems with moving boundaries and interfaces. The special space-time techniques are based on using, in the space-time flow
We present the core and special multiscale space–time (ST) methods we developed for thermo-fluid analysis of a ground vehicle and its tires. We also present application of these methods to thermo-fluid analysis of a freight truck and its rear set of tires. The core multiscale ST method is the ST variational multiscale (ST-VMS) formulation of the Navier–Stokes equations of incompressible flows with thermal coupling, which is multiscale in the way the small-scale thermo-fluid behavior is represent
Fluid–structure interaction (FSI) modeling of spacecraft parachutes involves a number of computational challenges beyond those encountered in a typical FSI problem. The stabilized space–time FSI (SSTFSI) technique serves as a robust and accurate core FSI method, and a number of special FSI methods address the computational challenges specific to spacecraft parachutes. Some spacecraft FSI problems involve even more specific computational challenges and require additional special methods. An examp
We present the space–time variational multiscale (ST-VMS) method for flow computations with slip interfaces (ST-SI). The method is intended for fluid–structure interaction (FSI) analysis where one or more of the subdomains contain spinning structures, such as the rotor of a wind turbine, and the subdomains are covered by meshes that do not match at the interface and have slip between them. The mesh covering a subdomain with the spinning structure spins with it, thus maintaining the high-resoluti
Abstract The stabilized space–time fluid–structure interaction (SSTFSI) technique developed by the team for advanced flow simulation and modeling is applied to the computation of arterial fluid–structure interaction (FSI) with patient‐specific data. The SSTFSI technique is based on the deforming‐spatial‐domain/stabilized space–time formulation and is supplemented with a number of special techniques developed for arterial FSI. These include a recipe for pre‐FSI computations that improve the conve
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