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This paper presents results of current DLR research on the stability and control behavior of a generic flying wing configuration. The geometry considered here is a flying wing configuration with a leading edge sweep angle of 53°. The focus of the in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::df7c5e01936330e50aec83ce31dce724
Autor:
Huber, Kerstin Claudie, Loeser, Thomas, Looye, Gertjan, Liersch, Carsten M., Lindermeir, Erwin, Kemptner, Erich, Klimmek, Thomas, Koch, Stefan, Kuchar, Richard, Nauroz, Mobin, Paul, Michael, Rein, Martin, Rode, Gerald, Rohlf, Detlef, Rütten, Markus, Schütte, Andreas, Schwithal, Jana, Siggel, Martin, Voss, Arne, Zimper, Dirk
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1640::13ae9d71a8b732966a65d8b35bad3d9e
https://elib.dlr.de/100733/
https://elib.dlr.de/100733/