Accession Number:

ADA129573

Title:

Combined Direct/Inverse Three-Dimensional Transonic Wing Design.

Descriptive Note:

Final rept. May 81-Sep 82,

Corporate Author:

LOCKHEED-GEORGIA CO MARIETTA

Report Date:

1983-05-01

Pagination or Media Count:

101.0

Abstract:

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

Subject Categories:

  • Theoretical Mathematics
  • Computer Programming and Software
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE