Exploratory Wind Tunnel Investigation Of Deployable Flexible Ventral Fins For Use As An Emergency Spin Recovery Device
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Exploratory Wind-tunnel Investigation of Deployable Flexible Ventral Fins for Use as an Emergency Spin-recovery Device
Spin-tunnel tests have been conducted on dynamic models of two fighter airplanes to explore the feasibility of using deployable flexible ventral fins as an emergency spin-recovery device. Various fin configurations, deflections, and locations were tested. The results indicated that the fins provided satisfactory spin recoveries for the models tested.