AIAA Aviation 2019 Forum 2019
DOI: 10.2514/6.2019-3598
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Aerodynamic and Transition Analysis of the Hybrid Laminar Flow ControlWing at ARA Wind Tunnel

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“…In the scope of a UK nationally funded research project ARA has also recently wind-tunnel tested a small-scale HLFC wing with a suction skin of variable porosity. While the HLFC design concept and scientific goals were somewhat different here, the documented observations in [7] confirm the beneficial application of variable against constant porosity for HLFC suction skins.…”
Section: Introductionmentioning
confidence: 57%
“…In the scope of a UK nationally funded research project ARA has also recently wind-tunnel tested a small-scale HLFC wing with a suction skin of variable porosity. While the HLFC design concept and scientific goals were somewhat different here, the documented observations in [7] confirm the beneficial application of variable against constant porosity for HLFC suction skins.…”
Section: Introductionmentioning
confidence: 57%