Applications of two- and three-dimensional interactive boundary-layer theory to finite wings with flow separation
25th AIAA Aerospace Sciences Meeting ; 1987 ; Reno , NV , U.S.A.
1987-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
A Three-Dimensional Boundary-Layer Method for Flow over Delta Wings with Leading-Edge Separation
SAE Technical Papers | 1985
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