Accession Number:
AD0750984
Title:
Ducted-Fan Turbojet Engines (Review of Development Based on Foreign Publications),
Descriptive Note:
Corporate Author:
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s):
Report Date:
1972-08-29
Pagination or Media Count:
19.0
Abstract:
The author analyzes operating principles and the thermodynamic cycle of turbofan rocket engines. Given is a brief analysis of the present state of turbofan rocket engines abroad, an analysis of design characteristics of a series of power plants, and basic diagrams of engines, their merits and shortcomings. Indicated are also the advantages of turbofan rocket engines at high supersonic-flight M numbers in comparison with other types of engines, as well as the possible field of application of turbofan rocket engines. Author
Descriptors:
Subject Categories:
- Jet and Gas Turbine Engines