Abstract
A time-parallel algorithm is developed for large-scale three-dimensional rotor dynamic analysis. A modified harmonic balance method with a scalable skyline solver forms the kernel of this algorithm. The algorithm is equipped with a solution procedure suitable for large-scale structures that have lightly damped modes near-resonance. The algorithm is integrated in X3D, implemented on a hybrid - shared and distributed memory architecture, and demonstrated on a three-dimensional structural model of a UH-60A-like fully articulated rotor. Flight test data from UH-60A Airloads Program transition flight C8513 are used for validation. The key conclusion is that the new solver converges to the time-integration solution more than 75 times faster, and achieves a performance of greater than 1 teraFLOPS. The significance of this conclusion is that the principal barrier of computational time for trim solution using high-fidelity three-dimensional structures can be overcome with the scalable harmonic balance method demonstrated in this paper.
Original language | English |
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Publication status | Published - 2020 |
Externally published | Yes |
Event | Vertical Flight Society's 76th Annual Forum and Technology Display - Virtual, Online Duration: 5 Oct 2020 → 8 Oct 2020 |
Conference
Conference | Vertical Flight Society's 76th Annual Forum and Technology Display |
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City | Virtual, Online |
Period | 5/10/20 → 8/10/20 |
ASJC Scopus subject areas
- Aerospace Engineering
- Control and Systems Engineering