PULSATING COMBUSTION OF GAS BEHIND A SHOCK WAVE IN SUPERSONIC FLOW,
Abstract
In the experiments described a shock tube was used to obtain a stream of mixture, in which the temperature behind the front of direct densification jump at the surface of the decelerating body is sufficient for adiabatic spontaneous combustion of the gas. The condition of periodic ignition of the gas behind the disconnected shock wave was investigated.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 13, 1965
- Accession Number
- AD0615985
Entities
People
- R. I. Soloukhin
Organizations
- National Air and Space Intelligence Center