Helicopter Gas Turbine Engines

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Scientific research is summarized and recommendations are given for improving the working process and design of helicopter gas turbine engines (GTD), their design, refinement, as well as for various types of tests and operation. The application of heat regeneration to increase the efficiency of the work process is considered , Methods of thermogas-dynamic calculation and calculation of characteristics , Interaction of the helicopter and its power plant , Assessment of the effectiveness of GTE in the aircraft system , Features of regulation, Forming a constructive image of the GTD and others. For engineering and technical workers of aircraft engine design bureaus, researchers, graduate students, students of aviation and technical universities .
LF/935182570/R
Data sheet
- Name of the Author
- Григорьев В.А.
Зрелов В.А.
Игнаткин Ю.М.
и др. - Language
- Russian
- ISBN
- 9785217033621
- Release date
- 2007