The Influence of Bypass Turbojet Engine Parameters on the Technical-Economic Characteristics of Long-Range Passenger Aircraft,
Abstract
The report describes parametric study of turbofan engines, intended for subsonic passenger main-liner aircraft with long flight range (up to 15,000 km) and increased passenger accommodation (up to 500 passengers). As a result of the study it is revealed the optimum values of parameters of operating conditions and the bypass ratio of turbofan engines, providing minimum values of takeoff weight of the aircraft and the smallest operating costs. In the study are also given data on the evaluation of the noise level of contemporary turbofan engines.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 10, 1973
- Accession Number
- AD0769316
Entities
People
- A. L. Klyachkin
- V. G. Enenkov
- Yu. D. Milenkii
Organizations
- National Air and Space Intelligence Center