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School of Engineering (SoE)
CoA. Reports
The performance of 60 degrees delta wings : the effects of leading edge radius on vortex flaps and the wing
The performance of 60 degrees delta wings : the effects of leading edge radius on vortex flaps and the wing
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COA_9004.PDF
(3.46 MB)
Date published
1990
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Authors
Hu, B. K.
Stollery, J. L.
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Cranfield Institute of Technology; College of Aeronautics
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Technical Report
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http://hdl.handle.net/1826/1080
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