  In this paper, the original discrete unified gas kinetic scheme (DUGKS) is
extended to arbitrary Lagrangian-Eulerian (ALE) framework for simulating the
low-speed continuum and rarefied flows with moving boundaries. For ALE method,
the mesh moving velocity is introduced into the Boltzmann-BGK equation. The
remapping-free scheme is adopted to develop the present ALE-type DUGKS, which
avoids the complex rezoning and remapping process in traditional ALE method. As
in some application areas, the large discretization errors will be introduced
into the simulation if the geometric conservation is not guaranteed. Three
compliant approaches of the geometric conservation law (GCL) are discussed and
a uniform flow test case is conducted to validate these schemes. To illustrate
the performance of present ALE-type DUGKS, four test cases are carried out. Two
of them are the continuum flow cases, which are the flows around the
oscillating circular cylinder and the pitching NACA0012 airfoil, respectively.
Others are the rarefied flow cases, one is the moving piston driven by the
rarefied gas, another is the flow caused by the plate oscillating in its normal
direction. The results of all test cases are in good agreement with the other
numerical and/or experimental results, demonstrating the capability of present
ALE-type DUGKS to cope with the moving boundary problems at different flow
regimes.
