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• W2161627873 abstract "Advanced Dynamics has developed an Integrated Variable-Fidelity Tool Set – ASTE-P for Modeling and Simulation of Aero-Servo-Thermo-Elasticity and Propulsion (ASTE-P) of Aerospace Vehicles Ranging from Subsonic to Hypersonic Flights. The ASTE-P software tool set is developed in the state-of-the-art and commercial standard and enables accurate integration and tight/loose coupling of the fluid, structural and control field simulation with variable fidelity options available. The ASTE-P software tool can be applicable to modeling and simulation of aerodynamics, structural dynamics, flight control and propulsion dynamics as well as more important interactions of these dynamics. All flight regimes from subsonic to hypersonic are covered. The interface of structural/control surface motion and vibration modes with fluid flows is modeled using either unified particle-based methods (MPM/PPM) or FVM/FEM based tight/loose coupled fluid/structure solving algorithms. The Euler and RANS based solvers enable the accurate prediction of nonlinear coupled fluidstructure problems in aeroelasticity and the embedded fluid and structural dynamics solvers make the software self-contained and not require the integration of two separate third-party fluid and structure solvers for aeroelastic modeling and simulation. Three levels of simulation environments are included in ASTE-P tool set: (1) the bottom level of high-fidelity and full-order simulation environment, (2) middle level of fast analysis and evaluation environment which is based upon reduced order models (ROM) and provides fast turn-around time, and (3) top level of rapid design and optimization environment. This paper provides the comprehensive validation and verification (V&V) of ASTE-P toolset recently done at Advanced Dynamics which resulted in over 600 pages report for over 40 benchmark test examples that were selected from industry and academic research and design . The validation cases presented in this paper indicate that the capability of ASTE-P is compatible or even more powerful than the similar software that is currently available." @default.
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• W2161627873 date "2011-04-04" @default.
• W2161627873 modified "2023-09-26" @default.
• W2161627873 title "ASTE-P: Integrated and Multi-fidelity Modeling and Simulation Tool for Aero-structure and Propulsion Dynamics of Aerospace Vehicles" @default.
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• W2161627873 doi "https://doi.org/10.2514/6.2011-2076" @default.
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