Prediction of laminar-turbulent transition on helicopter rotors in forward flight using the U/RANS solver TAU with an approximate boundary layer method
2016
v, 19, 32 Blätter
30 cm
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Digital preservation by Gottfried Wilhelm Leibniz Bibliothek - Niedersächsische Landesbibliothek
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Laminar boundary layers on helicopter rotors in forward flight
Engineering Index Backfile | 1968
|British Library Conference Proceedings | 1995
|British Library Conference Proceedings | 2013
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