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Verhaagen et al., 1995 - Google Patents

A study of the vortex flow over a 76/40-deg double-delta wing

Verhaagen et al., 1995

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Document ID
500312406976915102
Author
Verhaagen N
Jenkins L
Kern S
Washburn A
Publication year
Publication venue
33rd Aerospace Sciences Meeting and Exhibit

External Links

Snippet

Strake/wing configurations are employed for several modern peace keeping aircraft and for design concepts of high-speed civil transports (HSCT). The highly swept strake is an additional lifting surface above which a stable vortex is formed. This strake vortex persists …
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