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pro vyhledávání: '"K. V. Babarykin"'
Autor:
K. V. Babarykin
Publikováno v:
Journal of Engineering Physics and Thermophysics. 80:702-707
A transonic flow around a symmetric airfoil with a concavity in its central part has been numerically investigated. The dependences of the lift coefficient on the Mach number of the incident flow M∞ and on the angle of attack α were determined. It
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d5b66b3592d2eda9cd93c92f5a23f69c
https://doi.org/10.1007/s10891-007-0095-8
https://doi.org/10.1007/s10891-007-0095-8
