A shock wave suppression device is configured to suppress a shock wave generated on a blade surface of a blade, the shock wave suppression device including a bump cover provided to follow the blade surface and deformable to protrude outward from the blade surface, and a displacing unit configured to displace the bump cover between a steady state to follow the blade surface and a deformed state to protrude outward from the blade surface. The bump cover has a curved shape in the deformed state configured to be a continuous surface from an upstream side to a downstream side in a flow direction of a fluid flowing through the blade surface.
SHOCK WAVE SUPPRESSION DEVICE AND AIRCRAFT
19.08.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
SHOCK WAVE DETECTION SYSTEM, METHOD OF DETECTING SHOCK WAVE AND AIRCRAFT
Europäisches Patentamt | 2024
|SHOCK WAVE NOISE OF SUPERSONIC AIRCRAFT
SAE Technical Papers | 1960
|Shock wave noise of supersonic aircraft
Engineering Index Backfile | 1960
|