Design of a retrofit winglet for a transport aircraft with assessment of cruise and ultimate structural loads

Notes on Numerical Fluid Mechanics and Multidisciplinary Design

Volumn 96, Issue , 2007, Pages 62-70

  Streit, Th ^a   Himisch, J ^b   Heinrich, R ^a   Nagel, B ^b   Horstmann, K H ^a   Liersch, C ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b TECHNICAL UNIVERSITY OF BRAUNSCHWEIG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 35948978144     PISSN: 16122909     EISSN: None     Source Type: Book Series    
DOI: 10.1007/978-3-540-74460-3_8     Document Type: Conference Paper

References (9)

1. A. Mann, The M-DAW Project, Modelling and Design of Advanced Wing Tip Devices, CEAS/KATNET Conference on Key Aerodynamic Technologies, Conference Proceedings, June 2005, Bremen.
2. J.-L. Hantrais-Gervois, M. Rapin, Aerodynamic and Structural Behaviour of a Wing Equipped with a Winglet at Cruise, 44th AIAA Aerospace Science Meeting and Exhibit, January 2006, Reno, Nevada, AIAA 2006-1489
3. B.B. Prananta, A. Namer, J.E.J. Maseland, J. van Muijden, S.P. Spekreijse, Winglets on Large Civil Aircraft: Impact on Wing Deformation, International Forum on Aerolasticity and Structural Dynamics IFASD 2005, 2005.
4. K.-H. Horstmann: Ein Mehrfach-Traglinienverfahren und seine Verwendung für Entwurf und Nachrechnung nichtplanarer Flügelanordnungen, DVFLR-FB 87-51, 1987.
5. N. Kroll, J.K. Fassbender [Hrsg.]: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), 89, Springer Verlag, Closing Preparation DLR Project MEGAFLOW, 2002 Braunschweig.
6. B. Nagel., M. Rose, H.P. Monner, R. Heinrich: An Alternative Procedure for FE-Wing Modelling, Deutscher Luft- und Raumfahrtkongress Nov. 2006, Braunschweig, Germany.
7. R. Heinrich, J. Wild, Th. Streit., B. Nagel: Steady Fluid-Structure Coupling for Transport aircraft, Deutscher Luft- und Raumfahrtkongress 2006, Braunschweig.
8. G. Heller, P. Kreuzer, S. Dirmeier, T. Streit: Aerodynamische Untersuchung verschiedener Flügelseitenkanten-Erweiterungen der Envoy 7, Jahrbuch DGLR, Bd. III, pp. 1629-1634, 2002.
9. http://www.ansys.com