Flow past a delta wing with a sinusoidal leading edge: near-surface topology and flow structure

Overview of attention for article published in Experiments in Fluids, May 2009

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In the top 25% of all research outputs scored by Altmetric
Good Attention Score compared to outputs of the same age (72nd percentile)
Above-average Attention Score compared to outputs of the same age and source (57th percentile)

Mentioned by

patent: 9 patents

Citations

dimensions_citation: 63 Dimensions

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mendeley: 68 Mendeley

Summary Patents Dimensions citations

So far, Altmetric has seen 9 patents that reference this research output.

Vertical take off and landing closed wing aircraft

Grant US-11679877-B2

United States of America

Distributed propulsion system for vertical take off and landing closed wing aircraft

Grant US-11613355-B2

United States of America

Distributed propulsion system

Grant US-11603203-B2

United States of America

Vertical take off and landing closed wing aircraft

Grant US-10960978-B2

United States of America

Distributed propulsion system for vertical take off and landing closed wing aircraft

Grant US-10737786-B2

United States of America

Modular fuselage sections for vertical take off and landing distributed airframe aircraft

Grant US-10730624-B2

United States of America

Forward folding rotor blades

Grant US-10676183-B2

United States of America

Distributed propulsion system

Application US-10556680-B2

United States of America

VERTICAL TAKE OFF AND LANDING CLOSED WING AIRCRAFT

Application EP-3243747-A1

European Patent Office