AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM COMPATIBLE WITH A NATURAL LAMINAR FLOW WING WITHIN THE DESIREH PROJECT

机译：与自然层流翼相匹配的高升空系统的气动设计

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The paper describes the aerodynamic design ofa high lift system suitable for a Natural LaminarFlow wing. 2D & 3D numerical optimizationhas been used in the design process and theoutcome has been tested at flight ReynoldsNumber in the European Transonic Windtunnel(ETW), where various measurement techniqueshave been applied. An analysis on aircraft levelhas been performed to assess Natural LaminarFlow (NLF) wing’s drag benefits.

机译：本文介绍了汽车的空气动力学设计。适用于天然层流的高升力系统流动翼。 2D和3D数值优化已经在设计过程中使用，并且雷诺兹飞行的结果已经过测试欧洲跨音速风洞中的编号（ETW），其中各种测量技术已被应用。飞机高度分析已经进行了评估天然层流 Flow（NLF）机翼的阻力优势。

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《Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences》|2014年|1-8|共8页
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Henning Strüber; Jochen Wild;
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numerical optimization; flight Reynolds Number validation; Krueger; NLF;

机译：数值优化;;飞行雷诺数验证;; Krueger ;; NLF;

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专利

1. Simulation of Laminar-Flow Compatible High-Lift Wing Configuration with Flow Control [J] . Rizzetta Donald P., Visbal Miguel R. Journal of Aircraft . 2016,第5期

机译：层流兼容的高流量机翼配置及流量控制的仿真
2. High-lift design for a forward swept natural laminar flow wing [J] . D. Keller CEAS Aeronautical Journal . 2020,第1期

机译：前升式自然层流机翼的高升力设计
3. An inverse design method with aerodynamic design optimization for wing glove with hybrid laminar flow control [J] . Yang Yixiong, Bai Junqiang, Li Li, Aerospace science and technology . 2019,第Deca期

机译：具有混合层流控制的翼形手套的气动设计逆设计方法
4. AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM COMPATIBLE WITH A NATURAL LAMINAR FLOW WING WITHIN THE DESIREH PROJECT [C] . Henning Strüber, Jochen Wild Congress of the International Council of the Aeronautical Sciences . 2014

机译：高升降系统的空气动力学设计与Desenth项目中的天然层流翼兼容
5. Probabilistic inverse aerodynamic design optimization for natural laminar flow wings. [D] . Lee, Jae-Moon. 1999

机译：天然层流机翼的概率逆空气动力学设计优化。
6. Aerodynamic evaluation of wing shape and wing orientation in four butterfly species using numerical simulations and a low-speed wind tunnel and its implications for the design of flying micro-robots [O] . Alejandro Ortega Ancel, Rodney Eastwood, Daniel Vogt, 2017

机译：利用数值模拟和低速风洞对四种蝶类的翼形和翼向进行空气动力学评估及其对飞行微型机器人设计的启示
7. Aerodynamic performance of the DeSiReH high-lift laminar wing at free flight and ETW in-tunnel conditions [O] . S. Bosnyakov, E. Kazhan, I. Kursakov, 2015

机译：Walenth高升降层翼的空气动力学性能在自由飞行和ETW隧道条件下
8. Aerodynamic design considerations and theoretical results for a high Reynolds number natural laminar flow airfoil [R] . Viken, Jeffrey K. 1983

机译：高雷诺数自然层流翼型的空气动力学设计考虑和理论结果

AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM COMPATIBLE WITH A NATURAL LAMINAR FLOW WING WITHIN THE DESIREH PROJECT

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