Design and aeroelastic assessment of a forward-swept wing aircraft

Author:

Krüger Wolf R.,Klimmek Thomas,Liepelt René,Schmidt Hauke,Waitz Stefan,Cumnuantip Sunpeth

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference35 articles.

1. Mai, H., Hebler, A.: Aeroelasticity of a laminar wing. In: Proceedings of IFASD 2011—15th International Forum on Aeroelasticity and Structural Dynamics, 26–30 June 2011, Paris, France (2011)

2. Fehrs, M.: influence of transitional flows at transonic mach numbers on the flutter speed of a laminar airfoil. In: Proceedings IFASD 2013—16th International Forum on Aeroelasticity and Structural Dynamics, 24–27 June 2013, Bristol, UK (2013)

3. Schmidt, H., Neumann, J., Mai, H.: Analysis of forced response in a wind tunnel based on doublet-lattice method. CEAS Aeronaut. J. 2, 271–277. Springer. doi: 10.1007/s13272-011-0017-5 (2011)

4. Neumann, J., Mai, H.: Gust response: simulation of an aeroelastic experiment by a fluid-structure interaction method. J. Fluid Struct. 38(1), 290–302. Elsevier (2013)

5. Seitz, A., Kruse, M., Wunderlich, T., Bold, J., Heinrich, L.: The DLR project LamAiR: design of a NLF forward swept wing for short and medium range transport application. In: 29th AIAA Applied Aerodynamics Conference, 27–30, June 2011, Hawaii, USA (2011)

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