Analysis of computational aeroelastic simulations by fitting time signals
نویسندگان
چکیده
The procedures to assess the critical aeroelastic state of an aircraft with the AESIM simulation method are described. The main innovation is the identification with MIMO-class methods which opens up possibilities for efficient usage of aeroelastic simulation methods. Experience with recent applications is reported. ANALYSIS OF COMPUTATIONAL AEROELASTIC SIMULATIONS BY FITTING TIME SIGNALS Michael H.L. Hounjet and Bart J.G. Eussen NLR, Anthony Fokkerweg 2, 1059 CM Amsterdam email: [email protected] email: [email protected] Marco W. Soijer Faculty of Aerospace Engineering Delft University of Technology, Kluyverweg 1, 2629 HS Delft email: [email protected] Abstract. The procedures to assess the critical aeroelastic state of an aircraft with the AESIM simulation method are described. The main innovation is the identi cation with MIMO-class methods which opens up possibilities for e cient usage of aeroelastic simulation methods. Experience with recent applications is reported.
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