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Published in: Fluid Dynamics 1/2022

01-12-2022

Supersonic Flow over Annular Cavities at an Angle of Attack

Authors: S. V. Guvernyuk, M. M. Simonenko, A. F. Zubkov

Published in: Fluid Dynamics | Special Issue 1/2022

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Abstract

Results obtained for experimental studies on a supersonic flow over an axisymmetric cylindroconical body with an annular cavity of a rectangular axial cross section at an angle of attack and at Mach number M = 2.5 are presented. Data visualization of the flow structure, pressure measurements, and weight testing have been obtained for relative cavity lengths ranging from 6 to 18. The structure evolution and parameters of the flow over a cavity has been studied under a continuous change in the angle of attack in the range from ‒ 4° to 16°. Different flow modes corresponding to closed, open, and combined patterns of flow over a cavity have been identified. The existence ranges of aerodynamic hysteresis in the transition between flow modes from one pattern of flow over a cavity to another have been estimated in the space of dimensionless problem-determining parameters.

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Metadata
Title
Supersonic Flow over Annular Cavities at an Angle of Attack
Authors
S. V. Guvernyuk
M. M. Simonenko
A. F. Zubkov
Publication date
01-12-2022
Publisher
Pleiades Publishing
Published in
Fluid Dynamics / Issue Special Issue 1/2022
Print ISSN: 0015-4628
Electronic ISSN: 1573-8507
DOI
https://doi.org/10.1134/S0015462822601292

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