this article summarizes the capabilities and development of the helios version 2.0; or shasta; software for rotary wing simulations. specific capabilities enabled by shasta include off-body adaptive mesh refinement and the ability to handle multiple interacting rotorcraft components such as the fuselage; rotors; flaps and stores. in addition; a new run-mode to handle maneuvering flight has been added. fundamental changes of the helios interfaces have been introduced to streamline the integration of these capabilities. various modifications have also been carried out in the underlying modules for near-body solution; off-body solution; domain connectivity; rotor fluid structure interface and comprehensive analysis to accommodate these interfaces and to enhance operational robustness and efficiency. results are presented to demonstrate the mesh adaptation features of the software for the naca0015 wing; tram rotor in hover and the uh-60a in forward flight.;
机译:使用HPCMP CREATE-AV Helios进行基于原理的基于物理的旋翼飞机流场仿真
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机译:用于旋翼飞机仿真的Helios 2.0版计算平台概述
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