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- W2022595511 abstract "This paper addresses the development of aircraft models for flight loads analysis in the pre-design stage. The underlying model structure consists of the nonlinear equations of motion of a free flying, flexible aircraft, as well as a model, which calculates the distributed aerodynamics over the entire airframe. Different possibilities in modelling the unsteady arodynamic interactions for pre-design purposes are explored and the effects on the loads are compared in order to assess the tradeoffs between accuracy and speed." @default.
- W2022595511 created "2016-06-24" @default.
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- W2022595511 date "2005-06-19" @default.
- W2022595511 modified "2023-09-29" @default.
- W2022595511 title "Comparison of Unsteady Aerodynamic Modelling Methodologies with Respect to Flight Loads Analysis" @default.
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- W2022595511 doi "https://doi.org/10.2514/6.2005-6027" @default.
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