STAND FOR TESTING A GAS-TURBINE ENGINE,
Abstract
The proposed stand differs from those known in that the line contains a gas-intake duct with a baffle plate to select a portion of the hot gas, which permits regulation of the flow parameters at the inlet to the tested engine. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 08, 1970
- Accession Number
- AD0713041
Entities
People
- A. I. Zinin
- E. D. Stenkin
- E. M. Semenov
- N. D. Kuznetsov
- Ya. I. Dvorkin
Organizations
- National Air and Space Intelligence Center