Abstract
A study has been made of the possibility of controlling the aerodynamic characteristics of airfoils with the use of local pulse‐periodic energy supply to the flow near the contour of the airfoil in transonic modes of flight. The influence of energy supply of different intensity to the supersonic region on the structure of the flow and the wave resistance of the airfoil has been studied based on mathematical modeling. The flow is modeled based on the two‐dimensional unsteady equations of gas dynamics.
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
