Numerical Optimization of High Convoluted Serpentine Air Inlet Duct Using Response Surface Methodology | AVESİS

Middle East Technical University Research Information System

Numerical Optimization of High Convoluted Serpentine Air Inlet Duct Using Response Surface Methodology

Copy For Citation

YAHŞİ Ö. F., Yılmaz M. H., Günaydınlıoğlu E., ÖZYÖRÜK Y.

AIAA Aviation Forum 2023, San Diego, United States Of America, 12 June 2023

Publication Type: Conference Paper / Full Text
Doi Number: 10.2514/6.2023-3587
City: San Diego
Country: United States Of America
Middle East Technical University Affiliated: Yes