And Trailing-Edge Control on a Swept Lambda Wing Magnus Tormalm, Jean-François Le Roy, Stephane Morgand
Numerical Assessment of Leading- and Trailing-Edge Control on a Swept Lambda Wing Magnus Tormalm, Jean-François Le Roy, Stephane Morgand To cite this version: Magnus Tormalm, Jean-François Le Roy, Stephane Morgand. Numerical Assessment of Leading- and Trailing-Edge Control on a Swept Lambda Wing. Journal of Aircraft, American Institute of Aeronautics and Astronautics, 2018, 55 (2), pp.603-622. 10.2514/1.C033820. hal-02382423 HAL Id: hal-02382423 https://hal.archives-ouvertes.fr/hal-02382423 Submitted on 26 May 2021 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Numerical Assessment of Leading- and Trailing-Edge Control on a Swept Lambda Wing Magnus Tormalm∗ Swedish Defence Research Agency (FOI), SE-16490 Stockholm, Sweden and Jean-François Le Roy† and Stephane Morgand‡ ONERA–The French Aerospace Lab, FR-59045 Lille, France The next generation of agile unmanned combat aerial vehicles has put focus on the stability and control of low observable platforms. Without the traditional fin for yaw control combined with delta wings, a challenging task has been presented to the research community. The NATO research group AVT-201 was formed to meet this challenge and build on previous knowledge gained on the complex vortical flow of rounded leading-edge delta wings.
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