A Study of the Flow Around Plane and Axially Symmetrical Bodies with a Separated Shock Wave by a Flow at Low Supersonic Speed,
Abstract
This work is a continuation of the study of the flow around bodies of various forms by a supersonic flow of an ideal gas. G. F. Telenin's method for the integration of equations of gas dynamics is used in the calculation of the flow around plane and axially symmetrical bodies by a flow at low supersonic speed. Basically the range of mach numbers M <2 is examined. A comparison is carried out with experimental data and the results of calculations with the use of other numerical methods.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 06, 1974
- Accession Number
- ADA004442
Entities
People
- M. G. Lebedev
- S. M. Gilinskii
Organizations
- National Air and Space Intelligence Center