Numerical Modeling of the Effect of Supersonic Vortex Structures on the Heat Transfer on the Lifting Surfaces of Flight Vehicles

IF 1 4区工程技术 Q4 MECHANICS

Fluid Dynamics Pub Date : 2024-11-12 DOI:10.1134/S0015462824602997

V. E. Borisov, T. V. Konstantinovskaya, A. E. Lutskii

引用次数: 0

Abstract

The simultaneous flow past two rectangular tandem wings is considered. The heat loads on the main wing are studied as functions of the intensity of the vortex formations produced by a generator. The following flow regimes are considered; the freestream Mach number М_∞ = 3 and the attack angles of the generator are 10° and 20°. It is shown that under certain conditions the surface temperature of the main wing can be considerably reduced due to its interaction with vortex structures.

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来源期刊

Fluid Dynamics MECHANICS-PHYSICS, FLUIDS & PLASMAS

CiteScore

1.30

自引率

22.20%

发文量

审稿时长

6-12 weeks

期刊介绍： Fluid Dynamics is an international peer reviewed journal that publishes theoretical, computational, and experimental research on aeromechanics, hydrodynamics, plasma dynamics, underground hydrodynamics, and biomechanics of continuous media. Special attention is given to new trends developing at the leading edge of science, such as theory and application of multi-phase flows, chemically reactive flows, liquid and gas flows in electromagnetic fields, new hydrodynamical methods of increasing oil output, new approaches to the description of turbulent flows, etc.