Abstract: In our previous work on ultralow-aspect ratio transonic turbine inlet guide vanes (IGVs) for a small turbofan engine (, 2005, “ Three Dimensional Aerodynamic Optimization for an Ultra-Low Aspect ...

Abstract: The development of high-performance turbine airfoils has been investigated under the condition of a supersonic exit Mach number. In order to obtain a new aerodynamic design concept for a ...