Aerofoil with recess or recesses below and proximal to its leading edge extremity for increased lift and flow attachment, and for improved control of dynamic stall
A Provisional patent application filed on 29 April 2014 credited to Cameron, Michael John Vernon
Details
Application number :
2014901532
Application type :
Provisional
Application status :
LAPSED
Under opposition :
No
Proceeding type :
Invention title :
Aerofoil with recess or recesses below and proximal to its leading edge extremity for increased lift and flow attachment, and for improved control of dynamic stall