Investigation of Propagation and Orientation of the Turbojet Engine Reverse Jets to Reduce the Ingress of Exhaust Gases to the Engine Inlet

G. F. Mingaleev; A. V. Kosterin; A. A. Lopatin

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Investigation of Propagation and Orientation of the Turbojet Engine Reverse Jets to Reduce the Ingress of Exhaust Gases to the Engine Inlet

机译：Investigation of Propagation and Orientation of the Turbojet Engine Reverse Jets to Reduce the Ingress of Exhaust Gases to the Engine Inlet

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摘要

The results of experimental studies are presented that describe the propagation and orientation of reverse jets in the air cross flow in order to determine design parameters of deflection vane cascade for preventing the ingress of reverse jets in the own or nearby engine.

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来源
《Russian Aeronautics》 |2018年第4期|561-566|共6页
作者
G. F. Mingaleev; A. V. Kosterin; A. A. Lopatin;
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作者单位

Tupolev Kazan National Research Technical University;

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原文格式 PDF
正文语种英语
中图分类航空;
关键词
thrust reverse; reverse jet; wind tunnel; deflection vane cascade;

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Investigation of Propagation and Orientation of the Turbojet Engine Reverse Jets to Reduce the Ingress of Exhaust Gases to the Engine Inlet

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