The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack
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Author
Contributions
- Drougge, Georg. - Contributor
- Eliasson, Peter. - Contributor
- The Aeronautical Research Institute of Sweden - Contributor
Publication
1988 - Aeronautical Research Institute of Sweden, Stockholm
Subjects
Topics
Delta wingsSupersonic drag
Series Statement
- FFA meddelande -- 141
- FFA report -- 141
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