Abstract
AbstractThis chapter introduces the aerodynamic characteristics of transonic thin airfoil and wing. It includes the concept of critical Mach number of transonic airfoil flow, transonic thin airfoil flow phenomenon and aerodynamic characteristics, transonic small perturbation potential flow equation and similarity rule, the influence of wing geometric parameters on transonic critical Mach number, and aerodynamic characteristics of supercritical airfoil flow, high subsonic flow over a swept wing with a high aspect ratio and transonic area rule.
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Published version (
Free)
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
