Impact of frontal-porous-insert temperature on the cylinder drag in supersonic flow


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Abstract

In the present paper, we report on experimental and simulated data on the impact of cellular-porous-material heating on the wave drag of a cylinder with a frontal gas-permeable porous insert streamlined by a supersonic flow (М = 4.85, Re1∞ = 3.3×106 m-1). Weighing data obtained in the supersonic wind tunnel are compared with data simulated using a discrete model of the cellular-porous material. An increase of the wave drag with a growth of porous-insert temperature and its decrease occurring upon decreasing the temperature are demonstrated.

About the authors

S. G. Mironov

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS; Novosibirsk State University

Author for correspondence.
Email: mironov@itam.nsc.ru
Russian Federation, Novosibirsk; Novosibirsk

T. V. Poplavskaya

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS; Novosibirsk State University

Email: mironov@itam.nsc.ru
Russian Federation, Novosibirsk; Novosibirsk

S. V. Kirilovskiy

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS; Novosibirsk State University

Email: mironov@itam.nsc.ru
Russian Federation, Novosibirsk; Novosibirsk


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