Reverse Flow Aerodynamics of Low Reynolds Number Rotors with Blunt Trailing-Edged Blades at High Advance Ratios
AIAA SCITECH 2022 Forum
01.01.2022
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Reynolds Number Effects on Vortex Breakdown of a Blunt-Edged Delta
Online Contents | 1996
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