Evaluation of the noise impact of flap-tip fences installed on laminar wings

Author:

Burghignoli LorenzoORCID,Di Marco Alessandro,Centracchio Francesco,Camussi Roberto,Ahlefeldt Thomas,Henning Arne,Adden Stephan,Di Giulio Massimiliano

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference54 articles.

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2. Advisory Council for Aviation Research and Innovation in Europe (ACARE): Strategic, Research and Innovation Agenda Vol. 1, delivering Europe’s Vision for aviation (2017). http://www.acare4europe.org/sites/acare4europe.org/files/attachment/acare-strategic-research-innovation-volume-1-v2.7-interactive-fin_0.pdf . Accessed 3 June 2020

3. Moens, F., Capbern, P.: Design and testing of leading-edge high-lift device for laminar flow wing applications. In: Proceedings of Conference on High Lift and Separation Control, Royal Aeronautical Society, p. 7-1–7-13 (1995)

4. Burnside, N.J., Horne, W.C., Elmer, K.R., Cheng, R., Brusniak, L.: Phased acoustic array measurements of a 5.75 percent hybrid wing body aircraft. In: AIAA SciTech 2016, 4–8, : San Diego, CA, United States (2016)

5. Runyan, L. J., Bielak, G. W., Behbehani, R. Chen, A. W., Rozendaal, R. A.: 757 NLF Glove Flight Test and Results. In: Symposium on Natural Laminar Flow and Laminar Flow Control Research, NASA-Langley Research Center, NASA CP-2487, March 16–19, pp. 795-818 (1987)

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