Combined Direct/Inverse Three-Dimensional Transonic Wing Design.
Final rept. May 81-Sep 82,
LOCKHEED-GEORGIA CO MARIETTA
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A combined directinverse three-dimensional transonic wing design method is presented. The method is built around the ZEBRA II transonic potential flow solution algorithm to provide a design method that is particularly suited for use on a vector computer. The development of a pilot design computer code and a baseline designanalysis code is described. Results are presented that verify the accuracy and consistency of the design method. Author
- Theoretical Mathematics
- Computer Programming and Software
- Fluid Mechanics