Shock Tube with a Diffuser near Diaphragm,
Abstract
A consideration is given of various models of the gas flow in a shock tube with a diffuser in the range of low shock wave mach numbers. Expressions are derived which relate the shock wave intensity to the initial conditions in the high and low pressure chambers. A brief review is presented of the special features of the design of a device of this type. The preliminary experimental data obtained are compared with theoretical estimates.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 23, 1971
- Accession Number
- AD0738248
Entities
People
- B. A. Kuklin
- S. N. Isakov
- V. V. Grigorev
Organizations
- National Air and Space Intelligence Center