The Work of Turbine and Injection Burners on a Gas Variable Composition,
Abstract
Combustion and aerodynamic installations are described which are used to determine amount of air (gas to air ratios) required to burn fuels of different compounds in turbojet or injection burners. Equations were developed to calculate the air requirements in turbojet and injection systems when changing feed gases of known density and compositions. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1970
- Accession Number
- AD0719834
Entities
People
- B. P. Adinskov
- E. P. Shchurkin
- V. I. Korobko
Organizations
- National Air and Space Intelligence Center