FFVHC-ACE: fully automated Cartesian-grid-based solver for compressible large-eddy simulation
This study presents a fully automated Cartesian-grid-based compressible flow solver,
named FrontFlow/Violet Hierarchical Cartesian for Aeronautics based on Compressible-flow …
named FrontFlow/Violet Hierarchical Cartesian for Aeronautics based on Compressible-flow …
Comparison of simulated sonic boom in stratified atmosphere with flight test measurements
M Kanamori, T Takahashi, Y Makino, Y Naka… - AIAA Journal, 2018 - arc.aiaa.org
A method for predicting sonic boom waveforms emanating from a vehicle flying at
supersonic speed is presented and compared to flight-test data. The prediction is achieved …
supersonic speed is presented and compared to flight-test data. The prediction is achieved …
Challenges in unstructured mesh generation for practical and efficient computational fluid dynamics simulations
Y Ito - Computers & Fluids, 2013 - Elsevier
An efficient and robust unstructured mesh generator, the Mixed-Element Grid Generator in 3
Dimensions (MEGG3D), has been developed to create good-quality meshes quickly and …
Dimensions (MEGG3D), has been developed to create good-quality meshes quickly and …
JAXA's TAS-Code Results of Fixed Grid RANS Simulations for the Fifth High Lift Prediction Workshop
JAXA's fixed grid RANS simulations for the Fifth High Lift Prediction Workshop (HLPW-5) are
summarized. Using the TAS-code, an unstructured grid RANS solver with the Spalart …
summarized. Using the TAS-code, an unstructured grid RANS solver with the Spalart …
JAXA's Results of Fixed Grid RANS Simulations for the Fourth High Lift Prediction Workshop
M Murayama, Y Ito, R Furuya, K Tanaka - AIAA Aviation 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-3743. vid This paper summarizes
the Japan Aerospace Exploration Agency's studies for the fourth AIAA CFD High Lift …
the Japan Aerospace Exploration Agency's studies for the fourth AIAA CFD High Lift …
Wind Tunnel Installation Effects on Japan Aerospace Exploration Agency's Standard Model
Y Ito, M Murayama, Y Yokokawa, K Yamamoto… - Journal of Aircraft, 2022 - arc.aiaa.org
This paper investigates the interference effects of wind tunnel floor and walls on the Japan
Aerospace Exploration Agency's High-Lift Configuration Standard Model (JSM) as an …
Aerospace Exploration Agency's High-Lift Configuration Standard Model (JSM) as an …
Effect of vortex generators on transonic swept wings
Y Ito, K Yamamoto, K Kusunose, S Koike, K Nakakita… - Journal of Aircraft, 2016 - arc.aiaa.org
This paper examines the effects of corotating blade-type vortex generators on transonic
sweptback wings using computational fluid dynamics studies. Infinite-span (two …
sweptback wings using computational fluid dynamics studies. Infinite-span (two …
TAS code, FaSTAR, and Cflow results for the sixth drag prediction workshop
Y Ito, M Murayama, A Hashimoto, T Ishida… - Journal of Aircraft, 2018 - arc.aiaa.org
Three mixed-element unstructured Reynolds-averaged Navier–Stokes solvers, the TAS
code, FaSTAR, and Cflow, were applied to the Sixth AIAA Drag Prediction Workshop test …
code, FaSTAR, and Cflow, were applied to the Sixth AIAA Drag Prediction Workshop test …
3d fluid–structure interaction simulation with an Arbitrary–Lagrangian–Eulerian approach with applications to flying objects
Air-structure interaction is a key aspect to account for during the design of Micro Air Vehicles.
In this context, modelisation and numerical simulations represent a powerful tool to analyse …
In this context, modelisation and numerical simulations represent a powerful tool to analyse …
JAXA's and KHI's Contribution to the Third High Lift Prediction Workshop
Y Ito, M Murayama, Y Yokokawa, K Yamamoto… - Journal of Aircraft, 2019 - arc.aiaa.org
This paper is based on results presented at the Third High Lift Prediction Workshop. The
Japan Aerospace Exploration Agency provided computer-aided design models and …
Japan Aerospace Exploration Agency provided computer-aided design models and …