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Model Study of Conditions, when the Reverse Jet Ingests into the Engine Input Located Behind the Wing

机译:当反向射流摄入位于机翼后面的发动机输入时的条件模型研究

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摘要

This paper presents the results of the model studies of the reverse jet distribution limits in the air cross-flow, performed in the wind tunnel, as well as the conditions of the jet's ingestion into the engine air intake in the context of aircraft configuration, when the engines are the input of engines.
机译:本文介绍了在风洞中进行的空气错流中反向射流分布极限的模型研究结果,以及当发动机是发动机的输入时,在飞机配置的背景下,射流进入发动机进气口的条件。

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