Determining the Balancing Parameter for a Correcting Circuit Operating in a Gas Temperature Control System of a Gas-Turbine Aviation Engine,
Abstract
The report describes a numerical method for determining gas flow rates and gas temperatures in order to balance control systems of gas turbine engines.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 10, 1973
- Accession Number
- AD0768436
Entities
People
- I. P. Pelepeichenko
- V. G. Volkov
- Yu. N. Dotsenko
Organizations
- National Air and Space Intelligence Center