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
Diagramme
Literaturangaben
Digital preservation by Gottfried Wilhelm Leibniz Bibliothek - Niedersächsische Landesbibliothek
Report
English
British Library Conference Proceedings | 1995
|Laminar boundary layers on helicopter rotors in forward flight
Engineering Index Backfile | 1968
|