飞机超音速进气道气动设计的综合方法

IF 0.8 Q3 ENGINEERING, AEROSPACE

Aviation Pub Date : 2021-03-01 DOI:10.3846/AVIATION.2021.12327

A. Kornev, S. Stetsenko, V. Yatsenko, A. Smolyakov, D. Kalinichenko

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引用次数: 2

摘要

对飞机的超音速进气道进行了分析和实验研究。提出了一种综合的飞机超音速进气道气动设计方法，消除了小型风洞试验面积的尺度效应问题。该设计方法合理分配了数值实验和物理实验的任务，加快了开发进程，降低了资源强度。介绍了冲压发动机在超音速风洞中进气物理模型的独特试验结果。

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INTEGRATED APPROACH TO GAS-DYNAMIC DESIGNING OF SUPERSONIC AIR INTAKES OF AIRCRAFT

The analytical and experimental studies of the aircraft’s supersonic air intakes have been carried out. An integrated approach to the gas-dynamic designing of aircraft’s supersonic air intakes that eliminates the scale effect problem of a wind tunnel with a small-sized testing area is proposed. The designing approach accelerates the development process and reduces the resource intensity due to the rational distribution of tasks between numerical and physical experiments. The results of the unique tests of the scaled ramjet’s air intake physical model in the supersonic wind tunnel are presented.

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来源期刊

Aviation ENGINEERING, AEROSPACE-

CiteScore

2.40

自引率

10.00%

发文量

审稿时长

15 weeks

期刊介绍： CONCERNING THE FOLLOWING FIELDS OF RESEARCH: ▪ Flight Physics ▪ Air Traffic Management ▪ Aerostructures ▪ Airports ▪ Propulsion ▪ Human Factors ▪ Aircraft Avionics, Systems and Equipment ▪ Air Transport Technologies and Development ▪ Flight Mechanics ▪ History of Aviation ▪ Integrated Design and Validation (method and tools) Besides, it publishes: short reports and notes, reviews, reports about conferences and workshops