Axial Impact of a Cylindrical Shell on the Surface of Compressible Fluid,
Abstract
The article considers the impact of a thin elastic shell of circular cross section, with a rigid flat leading edge and fluid filler, against the horizontal surface of a quiescent compressible fluid. The velocity of the impact is directed along the axis of the shell perpendicularly to the surface of the fluid.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 07, 1973
- Accession Number
- AD0763259
Entities
People
- A. Ya. Sagomonyan
Organizations
- National Air and Space Intelligence Center