Prediction of Shock Angles Caused by Sharp Delta Wings with Attack Angle
Copyright policy ) S. Koide; A. F. Loria; H. Babinsky;
Prediction of Shock Angles Caused by Sharp Delta Wings with Attack Angle
Using a combined method, one can specify the trace of the shock generated by a swept sharp fin on the wall for various angles of attack α, sweep angles λ, half-apex angles e, and Mach numbers M
- University of Cambridge United Kingdom
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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).
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This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
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