Abstract
This paper describes numerical methods which can be used for the computation of the motion of plates when subjected to large transient pressure pulses. The methods are based on an Eulerian formulation of the physical conservation laws which are integrated by high order accurate methods. The boundaries of an inclined plate are followed in time by an interface fitting procedure. Boundary layer effects due to severe plate distortions are resolved by solving the problem in a transformed plane which is obtained by stretching and rotating the coordinates of the physical plane. Some preliminary results are presented.
| Original language | English |
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| State | Published - 1972 |
| Event | Army Symp on Solid Mech, 3rd Bienn Meet, Proc - Ocean City, MD, USA Duration: 3 Oct 1972 → 5 Oct 1972 |
Conference
| Conference | Army Symp on Solid Mech, 3rd Bienn Meet, Proc |
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| City | Ocean City, MD, USA |
| Period | 3/10/72 → 5/10/72 |