INTEGRATED APPROACH TO GAS-DYNAMIC DESIGNING OF SUPERSONIC AIR INTAKES OF AIRCRAFT-Reference-Cited by-同舟云学术

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

Published:2021-03-01 Issue:1 Volume:25 Page:1-9
ISSN:1648-7788
Container-title:Aviation
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Author:

Kornev Aleksey¹^ORCID,Stetsenko Sergii¹^ORCID,Yatsenko Victor¹^ORCID,Smolyakov Anatoliy¹^ORCID,Kalinichenko Dmytro²^ORCID

Affiliation:

1. Inter-branch scientific research institute of problems of physical simulation of Zhukovsky National Aerospace University “Kharkov Aviation Institute” “KhAI” (NII PFM KhAI), Kharkiv, Ukraine

2. ““Yuzhnoye” Yangel Design Office” State Enterprise (““Yuzhnoye” DO” SE), Dnipro, Ukraine

Abstract

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.

Publisher

Vilnius Gediminas Technical University

Subject

Aerospace Engineering

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