An integrated capability for the preliminary design of aeroelasticity tailored wings
- 16 August 1976
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Estimation of transonic aircraft aerodynamics to high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975