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Autor:
Roos, Tobias
The problem presented in this report is that of finding a method to calculate the lift force from a single-element airfoil of arbitrary shape. A number of restrictions are used in order to simplify calculations while retaining reasonable accuracy. Th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::61cd0fab84b9ce2997fcf16c42f79b85
http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-47168
http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-47168
