Aeroelasticity & Structural Dynamics in a Fast Changing World
17 – 21 June 2024, The Hague, The Netherlands
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On the preparation of a flexible real-time aircraft model for a flight simulator


Go-down ifasd2024 Tracking Number 195

Presentation:
Session: Poster session & drinks
Room: Room 1.1
Session start: 18:00 Tue 18 Jun 2024

Gefferson Silva   g.silva@tu-berlin.de
Affifliation: Technische Universität Berlin

Bernd Boche   bernd.boche@tu-berlin.de
Affifliation: Technische Universität Berlin

Hannes Wilke   h.wilke@tu-berlin.de
Affifliation: Technische Universität Berlin

Flavio Silvestre   flavio.silvestre@tu-berlin.de
Affifliation: Technische Universität Berlin


Topics: - Computational Aeroelasticity (High and low fidelity (un)coupled analysis methods:), - Reduced Order Modeling (High and low fidelity (un)coupled analysis methods:)

Abstract:

Before flight test campaigns are pursued, handling qualities analyses of new aircraft designs are typically performed by means of a pilot-in-the-loop full-flight simulator. This also includes the forthcoming generation of greener aircraft, for which environmental damages resulting from aircraft emissions is mitigated. However, this type of air-vehicle requires special treatment in flight dynamics modeling and simulation, due to the interactive coupling between rigid-body dynamics and aeroelasticity. The extended model simulations result in an expressive increase in computational costs, which makes real-time simulations of flexible aircraft a current challenge. Therefore, the work at hand discusses an approach to reduce the computational consumption required for simulating slightly flexible aircraft models, in order to be embedded into a flight simulator. The mean-axes formulation is used to represent the coupled relations between flight mechanics and flexibility effects. The incremental forces and moments expressions are then modified algebraic-wise to obtain an equivalent but computationally efficient formulation to those expressions.