TRANSITION OF A COMBUSTION MIXTURE FROM SUPERSONIC FLOW TO THE CHAPMAN-JOUGET REGIME,
Abstract
The investigation of supersonic flow about bodies by a combustion mixture of gases is of importance in studying combustion efficiency of fuel in ramjet engines. In the present study, a numerical method is presented for solving the problem of supersonic flow about a cylinder and a plate with a cylindrical bluntness. A study was also made of a possible transition to the Chapman-Jouget regime.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 30, 1968
- Accession Number
- AD0681597
Entities
People
- S. M. Gilinskii
- Z. D. Zapryanov
Organizations
- National Air and Space Intelligence Center