CALCULATION OF HEAT FLUXES IN THE FLOW OF TWO DIFFERENT SUPERSONIC STREAMS AROUND A SHOULDER,
Abstract
A method is dealt with for determining the base enthalpy (or base temperature) in the flow around a flat or ring-shaped shoulder by two supersonic streams differing by the numbers M, full pressures and enthalpies of retardation. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 27, 1964
- Accession Number
- AD0605798
Entities
People
- R. K. Tagirov
Organizations
- National Air and Space Intelligence Center