A diamond-wing configuration has been developed to isolate and study blunt-leading edge vortex separation with both computations and experiments. The wing has been designed so that the results are relevant to a more complex Uninhabited Combat Air Vehicle concept known as SACCON. The numerical and theoretical development process for this diamond wing is presented, including a view toward planned wind tunnel experiments. This work was conducted under the NATO Science and Technology Organization, Applied Vehicle Technology panel. All information is in the public domain.
Numerical and Theoretical Considerations for the Design of the AVT-183 Diamond-Wing Experimental Investigations
AIAA 2015 SciTech
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2015
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Kissimmee, FL, United States
AIAA Aerospace Sciences Conference
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2015
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Kissimee, FL, United States
2015-01-05
Aufsatz (Konferenz)
Keine Angabe
Englisch
British Library Conference Proceedings | 2015
|Wing design with attainable thrust considerations
AIAA | 1984
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