An assembly is provided for an aircraft propulsion system. This assembly includes a nacelle exterior skin and a strake. The strake is configured with a base and an airfoil that projects out from the base. The base is recessed into and connected to the nacelle exterior skin.
STRAKE FOR AIRCRAFT PROPULSION SYSTEM NACELLE
2018-11-22
Patent
Electronic Resource
English
NUMERICAL INVESTIGATION AERODYNAMICS NACELLE-STRAKE EFFECT
British Library Conference Proceedings | 2018
|VORTEX CONTROL ON ENGINE NACELLE STRAKE AND OTHER VORTEX GENERATORS
European Patent Office | 2021
|