An inverse numerical technique for designing transonic airfoils having a prescribed pressure distribution is presented. The method uses the full potential equation, inverse boundary conditions, and Cartesian coordinates. It includes simultaneous airfoil update and utilizes a direct-inverse approach that permits a logical method for controlling trailing edge closure. The method can also be used for the analysis of flowfields about specified airfoils. Comparison with previous results shows that accurate results can be obtained with a Cartesian grid. Examples show the application of the method to design aft-cambered and other airfoils specifically for transonic flight.
Transonic airfoil analysis and design using Cartesian coordinates
Computational Fluid Dynamics Conference, 2nd ; 1975 ; Hartford, CN
1975-01-01
Miscellaneous
No indication
English
Transonic airfoil design using Cartesian coordinates
NTRS | 1976
|Transonic Airfoil Design Using Cartesian Coordinates
NTIS | 1976
|Transonic airfoil design using Cartesian coordinates
TIBKAT | 1975
|Transonic airfoil flowfield analysis using Cartesian coordinates
TIBKAT | 1975
|