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High-Order Shock Fitting with Finite Element MethodsA moving-grid, shock-tracking, finite element method has been implemented that can achieve high-order accuracy for flow simulations with shocks. In this approach, element edges in the computational mesh are fitted to the shock front and moved with the shock throughout the simulation. The Euler equations are solved on the moving mesh in an arbitrary Lagrangian-Eulerian framework. Three different methods for specifying the shock motion have been tested,and the order of accuracy of the resulting solutions was verified. It was found that one of the methods is applicable only for problems with a constant upstream flow state, whereas the other two methods converge to the expected solution for general shock problems. When using a finite element method with polynomial degree p, the two general shock motion methods converged with the expected order of accuracy of (p+1). Finally, accurate solutions are obtained for supersonic nozzle and blunt body bow shock problems. Based on the results, it is concluded that the shock tracking method can preserve high-order solution accuracy in the vicinity of a shock wave.
Document ID
20205002191
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Luke D'Aquila
(Clarkson University Potsdam, New York, United States)
Brian Helenbrook
(Clarkson University Potsdam, New York, United States)
Alireza Mazaheri
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 13, 2020
Subject Category
Engineering (General)
Meeting Information
Meeting: 2020 AIAA Aviation
Location: Reno, NV
Country: US
Start Date: June 15, 2020
End Date: June 19, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 394364.04.24.23.01
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
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