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The Effect of the Sweep Angle to the Turbulent Flow Past an Infinite Wing

Suardi, C., Pinelli, A. ORCID: 0000-0001-5564-9032 & Omidyeganeh, M. ORCID: 0000-0002-4140-2810 (2020). The Effect of the Sweep Angle to the Turbulent Flow Past an Infinite Wing. In: García-Villalba, M., Kuerten, H. & Salvetti, M. (Eds.), Direct and Large Eddy Simulation XII. DLES 2019. (ERCOFTAC Series). (pp. 321-327). Cham, Switzerland: Springer. doi: 10.1007/978-3-030-42822-8_42

Abstract

Nowadays the majority of civil aircraft employs swept-back wings. This configuration, proposed in the early 30s of last century, has been technologically motivated by the otherwise enhanced drag experienced in transonic cruise condition.

Publication Type: Book Section
Additional Information: The final authenticated version is available online at https://doi.org/10.1007/978-3-030-42822-8_42
Subjects: Q Science > QC Physics
T Technology > TL Motor vehicles. Aeronautics. Astronautics
Departments: School of Science & Technology > Engineering > Mechanical Engineering & Aeronautics
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