Further analysis of high-rate rolling experiments of a 65-deg delta wing
- 1 November 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 31 (6) , 1350-1357
- https://doi.org/10.2514/3.46658
Abstract
No abstract availableKeywords
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