Modeling the Flow around a Delta Wing Partially Made of a Permeable Material

Mathematical modeling of a supersonic gas flow around a delta wing is carried out for M = 2. A wing made of a conventional solid material is compared to a wing whose leading edge is made of a porous material with a porosity coefficient of 0.6. The influence of a permeable edge on the flow structure...

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Veröffentlicht in:	Fluid dynamics 2024-08, Vol.59 (4), p.1004-1015
Hauptverfasser:	Lutsky, A. E., Severin, A. V.
Format:	Artikel
Sprache:	eng
Schlagworte:	Classical and Continuum Physics Classical Mechanics Delta wings Engineering Fluid Dynamics Fluid- and Aerodynamics Gas flow Permeability Physics Physics and Astronomy Porous materials
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Zusammenfassung:	Mathematical modeling of a supersonic gas flow around a delta wing is carried out for M = 2. A wing made of a conventional solid material is compared to a wing whose leading edge is made of a porous material with a porosity coefficient of 0.6. The influence of a permeable edge on the flow structure and thermal regime is studied.
ISSN:	0015-4628 1573-8507
DOI:	10.1134/S0015462824602778