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 |
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Official URL: http://dx.doi.org/10.1007/978-3-030-42822-8_42
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