Analysis of the Effectiveness of Different Methods of the Adjustment of Parameters of a Twin-Shaft Turbojet Engine,
Abstract
Analysis of the comparative quality of plotting the parameters of a two shaft turbojet engine by varying the r.p.m. in the low pressure cascade during plotting, or the passage cross section of the jet nozzle, or the areas of the nozzle system passage cross sections in the first and second cascades of the turbine. These plotting techniques are applied in correcting the thrust, specific fuel consumption, gas temperature and compressor steady performance margin of a turbojet engine of this type. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 04, 1972
- Accession Number
- AD0749058
Entities
People
- A. M. Akhmedzyanov
- A. S. Tikhonov
- V. P. Alatortsev
Organizations
- National Air and Space Intelligence Center