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.
Cite
CITATION STYLE
APA
Suardi, C. A., Pinelli, A., & Omidyeganeh, M. (2020). The Effect of the Sweep Angle to the Turbulent Flow Past an Infinite Wing. In ERCOFTAC Series (Vol. 27, pp. 321–327). Springer. https://doi.org/10.1007/978-3-030-42822-8_42
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