Aerodynamic interference of airfoils in a subsonic unsteady flow
Copyright policy ) V. B. Kurzin;
Aerodynamic interference of airfoils in a subsonic unsteady flow
Integral equations [1] are used to study the case of unsteady gas flow about a system consisting of a finite number of airfoils. As an example, the aerodynamic forces acting on the airfoils of a biplane in an unsteady subsonic gas flow are calculated. In this very simple case, a special study is made of the acoustic resonance effect reported previously in [1, 2].
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selected citations
Citations provided by BIP!
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
Citations provided by BIP!popularityPopularity provided by BIP!
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
Popularity provided by BIP! 6
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Top 10%
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