Numerical investigations on the VFE 2 65-Degree rounded leading edge delta wing using the unstructured DLR-TAU-Code
46th, Aerospace sciences meeting AIAA ; 2008 ; Reno, NV
2008-01-01
17 pages
Conference paper
English
Aerospace , AIAA , Aeronautics , Astronautics
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Flow Field Around Thick Delta Wing with Rounded Leading Edge
SAE Technical Papers | 1991
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