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Type: Abstract
Information: The Aeronautical Journal , Volume 44 , Issue 350 , February 1940 , pp. 195 - 217

DOI: https://doi.org/10.1017/S0368393100103700 [Opens in a new window]

References

* Ωb/2V = spin coefficient where

Ω = resultant angular velocity,

b = span of wing,

V = rate of descent.

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Abstracts from the Scientific and Technical Press

Volume 44, Issue 350
DOI: https://doi.org/10.1017/S0368393100103700

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Abstracts from the Scientific and Technical Press

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