Effect of porous inserts on aerodynamics of flying vehicles

Author:

Maslov A A,Mironov S G,Poplavskaya T V,Kirilovskiy S V,Tsyryulnikov I S

Abstract

Abstract Experimental and numerical investigations of a supersonic flow around a cylindrical model with a porous frontal insert made of a high-porosity cellular material performed at the Khristianovich Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences are briefly reviewed. New data on the influence of the angle of attack on the flow around a cylinder with a porous frontal insert are reported. Methods of using high-porosity cellular materials for controlling supersonic flows around axisymmetric bodies are demonstrated.

Publisher

IOP Publishing

Subject

General Physics and Astronomy

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Shock-wave structures control methods in the input section of the aircraft high-speed air intake;Engineering Journal: Science and Innovation;2023-02

2. Analytical study of the possibilities of controlling the parameters of shocks in supersonic flow around gas-permeable bodies;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023

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