Computation of the steady viscous flow over a tri-element 'augmentorwing' airfoil
- 11 January 1982
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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- The transonic multi-foil Augmentor-WingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
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