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Integrated and Multi-fidelity Software Package for Aero- Servo-Thermo-Elasticity and Propulsion (ASTE-P) of Aerospace Vehicles from Subsonic to Hypersonic Flight

机译:集成和多保真软件包,用于亚音速飞行到高超音速飞行的航空航天器的航空伺服热弹性和推进(ASTE-P)

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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. AH 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/RANS/LES/DES solvers enable the accurate prediction of nonlinear coupled fluid-structure 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. In several our previous AIAA papers we have reported the integrated framework of ASTE-P and some validation cases, and in this paper we will update the status and enhancement of the ASTE-P recently, and present some new cases we have run to demonstrate that the functionalities of ASTE-P are compatible or even more efficient than the similar software that is currently available.
机译:Advanced Dynamics已开发出一种集成的可变保真度工具集-ASTE-P,用于对从亚音速飞行到高超音速飞行的航天飞机的航空-伺服-热弹性和推进(ASTE-P)进行建模和仿真。 ASTE-P软件工具集是根据最新的商业标准开发的,可实现流体,结构和控制场模拟的精确集成和紧密/松散耦合,并提供可变的保真度选项。 ASTE-P软件工具可用于空气动力学,结构动力学,飞行控制和推进动力学以及这些动力学更重要的相互作用的建模和仿真。涵盖了从亚音速到高音速的AH飞行方案。使用统一的基于粒子的方法(MPM / PPM)或基于FVM / FEM的紧密/松散耦合的流体/结构求解算法对结构/控制表面运动和振动模式与流体流动的界面进行建模。 Euler / RANS / LES / DES解算器可以准确预测气动弹性耦合的流体结构问题,而嵌入式流体和结构动力学解算器使该软件自成一体,无需集成两个单独的第三方流体和结构气动弹性建模和仿真的求解器。 ASTE-P工具集中包括三个级别的仿真环境:(1)高保真和全阶仿真环境的底层;(2)基于降阶模型的快速分析和评估环境的中等级别( ROM),并提供快速的周转时间,以及(3)顶级的快速设计和优化环境。在之前的几篇AIAA论文中,我们报告了ASTE-P的集成框架和一些验证案例,并且在本文中,我们将更新ASTE-P的状态和增强功能,并介绍一些新案例来证明这一点。 ASTE-P的功能与当前可用的类似软​​件兼容,甚至效率更高。

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