2019
DOI: 10.1007/978-3-030-25253-3_19
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Validation Experiment on a Passive Suction Flap for Hybrid Laminar Flow Control Applications

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(2 citation statements)
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“…In the scope of the project AFLoNext, a more advanced flap placed near the leading edge underneath the suction panel has been designed [17] and flight tested [6]. Although this flap is designed for high subsonic Mach numbers, the general principle of operation does not change to low speed, only the flaps efficiency increases [18]. The same flap geometry was, therefore, also integrated into the VER 2 SUS VTP model.…”
Section: Redesigned Passive Suction Flapmentioning
confidence: 99%
See 1 more Smart Citation
“…In the scope of the project AFLoNext, a more advanced flap placed near the leading edge underneath the suction panel has been designed [17] and flight tested [6]. Although this flap is designed for high subsonic Mach numbers, the general principle of operation does not change to low speed, only the flaps efficiency increases [18]. The same flap geometry was, therefore, also integrated into the VER 2 SUS VTP model.…”
Section: Redesigned Passive Suction Flapmentioning
confidence: 99%
“…Fig 18. Boundary layer state (laminar/turbulent) visualization with and without HLFC operation comparing the chamberless ("VarPoHyL") to the ALTTA ("VER 2 SUS") concept.…”
mentioning
confidence: 99%