Characteristics of Diffusers in Shock Tube,
Abstract
A study was done on diffuser starting in a shock tube at M=8 at variable Re numbers, and the throttling characteristics were recorded.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 23, 1974
- Accession Number
- AD0780376
Entities
People
- D. K. Roitenburg
- G. I. Kozlov
- V. M. Anufriev
Organizations
- National Air and Space Intelligence Center