The aerodynamic design process for transonic shock-free airfoils using the analytical hodograph theory is sketched. A user-oriented outline of the developed program system is presented. A number of examples of computed airfoils show that the computer program package provides final results of sufficient accuracy at acceptable costs and seems flexible enough to cover a wide range of engineering applications.
An Introductory Description of a Hodograph Method for Transonic Shock-Free Aerofoil Design
1973
43 pages
Report
Keine Angabe
Englisch