THE MEASUREMENT OF THE INITIAL GAS TEMPERATURE IN GT (GAS TURBINE) BASED ON INDIRECT PARAMETERS,
Abstract
The results of an investigation regarding the possible measurement of the initial gas temperature in a gas turbine through indirect parameters such as the final temperature of the gas after the turbine and the degree of expansion, are presented. The theoretical concepts supporting the application of this method and the corresponding technical approaches are included. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 26, 1968
- Accession Number
- AD0686236
Entities
People
- L. V. Arsenev
- S. A. Kantor
Organizations
- National Air and Space Intelligence Center