Internship student: Vidyut Balaji
Duration: June 6, 2022 – August 12, 2022
Supervisor: Yusuke Takahashi
Trainer(s) in Lab.: Mr. Sanjoy Saha
Research Title: Fluid-structure interaction of a Flat-Plate Wing in a High-Enthalpy Flow
Objectives: To investigate fluid-structure interaction and limit cycle oscillation behavior of thin flat wing using computational science approach
Analysis Target: Flat plate wing at transonic/subsonic speed
Learnings expected:
- To learn software programs and computer scripts related to fluid-structure interaction (FSI) analysis (C/C++, Python, Shellscript)
- To develop research skills and methodology related to FSI analysis
- To learn basic theory for fluid dynamics, structural mechanics, and computational engineering.
Tools:
- FSI software: SU2, CalculiX and preCICE (C/C++, Fortran)
- Preprocess/postprocess software: Pointwise, FreeCAD, Paraview
- Linux OS (Ubuntu)
- Interactive program for data processing and calculation operation: Python and Shellscript etc
- Office tool: Microsoft office (MS Word, Excel, and Powerpoint) and/or Mac office
- Cloud server:
- Storage server:
Project fSTEP:
Link: https://f3.eng.hokudai.ac.jp/self-evaluation-program-guide.html
Schedule planned:
1. First week (June 6—10, 2022)
- Definition of objectives of the present project through fSTEP of f3 center: https://f3.eng.hokudai.ac.jp/self-evaluation-program-guide.html
- Literature review study
- Accessing to cloud server in Hokkaido University
- Tutorials of preprocess/postprocess software: Pointwise, FreeCAD, and Paraview
2. Second 2 weeks (June 13—24 2021)
- Verification and validation of the present FSI analysis model (1)
- Reference: Attar et al., “Aeroelastic prediction of the limit cycle oscillations of a cropped delta wing”, Journal of Fluids and Structures 22 (2006) 45–58.
- Generating computational grids for flow field and structural mechanics simulations
- Setting computation setups for flow field and structural mechanics solvers, and coupler, for example, the boundary conditions initial conditions, and coupling schemes.
3. Third 2 weeks (June 27—July 8, 2022)
- Verification and validation of the FSI analysis model (2)
- Running FSI simulation for elastic wing on cloud server
- Postprocess of simulation results
- Comparison between the present FSI analysis results and referenced data (Attar’s paper)
4. Fourth 2 weeks (July 11—22, 2022)
- FSI analysis for flat wing
- Generating computational grids for flow field and structural mechanics simulations
- Setting computation setups for flow field and structural mechanics solvers, and coupler, for example, the boundary conditions initial conditions, and coupling schemes.
5. Fifth 2 weeks (July 25—August 5, 2022
- Running FSI simulation for elastic wing on cloud server
- Postprocess of simulation results
6. Fourth week (August 8–12, 2021)
- Conclusion of the internship study
- Technical report (final report)
References
- T.D. Economon, F. Palacios, S.R. Copeland, T.W. Lukaczyk, and J.J. Alonso. “SU2: An open-source suite for multiphysics simulation and design”. Aiaa Jour- nal, 54(3):828–846, 2016.
- G. Dhondt and K. Wittig. “Calculix a free software three-dimensional structural finite element program”. www.calculix.de.
- H.J. Bungartz, F. Lindner, B. Gatzhammer, M. Mehl, K. Scheufele, A. Shukaev, and B. Uekermann. “preCICE–a fully parallel library for multi-physics surface coupling”. Computers & Fluids, 141:250–258, 2016.
- preCICE”. https://github.com/precice.
- O.O. Bendiksen. “Review of unsteady transonic aerodynamics: Theory and applications”. Progress in Aerospace Sciences, 47(2):135–167, 2011.
- Y. Takahashi, Numerical Simulation of Fluid-Structure Interaction for Thin Flat Delta Wing at Transonic Speed based on Opensource Software, in: 9th edition of the International Conference on Computational Methods for Coupled Problems in Science and Engineering (COUPLED PROBLEMS 2021). URL https://www.scipedia.com/public/Takahashi_2021a
- Thomas Richter, Fluid-structure Interactions: Models, Analysis and Finite Elements (Lecture Notes in Computational Science and Engineering, 118) (if possible)
- Attar et al., “Aeroelastic prediction of the limit cycle oscillations of a cropped delta wing”, Journal of Fluids and Structures 22 (2006) 45–58.