Wind Tunnel Walls Effects on the NASA High Lift Common Research Model in RANS Calculations using FaSTAR

Kosuke Uchida; Tomoaki Matsuzaki; Yoimi Kojima; Andrea Sansica; Markus Zauner; Atsushi HASHIMOTO

doi:10.20637/0002000237

January 30, 2024Open Access

Wind Tunnel Walls Effects on the NASA High Lift Common Research Model in RANS Calculations using FaSTAR

View Full Paper

Ask AI

Bookmark

Share

Key Points

To assess how wind tunnel wall configurations affect the performance of the NASA High Lift Common Research Model in fluid dynamics simulations.
Utilized RANS (Reynolds-Averaged Navier-Stokes) calculations
Conducted simulations using the FaSTAR software
Analyzed various wind tunnel wall designs
Identified notable variances in aerodynamic performance based on wall effects
Demonstrated the importance of wall configurations in accurate fluid dynamics modeling

Ask about this paper

Answers are grounded in this paper and cite their sources.

Implication

Workshop reports effects of wind tunnel walls on high lift model performance using RANS calculations, suggesting important implications for aerospace design.

Abstract

No abstract yet. The journal hasn't published one we can show.

Discussion

No takes yet. Share an insight, caveat, or question.

Cite This Study

Uchida et al. (2024) studied this question.

synapsesocial.com/papers/69cd7aa45652765b073a7fa3 https://doi.org/10.20637/0002000237

View Full Paper

Ask AI

Bookmark

Share

Wind Tunnel Walls Effects on the NASA High Lift Common Research Model in RANS Calculations using FaSTAR

Key Points

Ask about this paper

Implication

Abstract

Discussion

Cite This Study

Wind Tunnel Walls Effects on the NASA High Lift Common Research Model in RANS Calculations using FaSTAR

Key Points

Ask about this paper

Implication

Abstract

Discussion

Cite This Study

Keep reading

Keep reading