Suscripción a Biblioteca: Guest
Portal Digitalde Biblioteca Digital eLibros Revistas Referencias y Libros de Ponencias Colecciones
TsAGI Science Journal

ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604

TsAGI Science Journal

DOI: 10.1615/TsAGISciJ.v41.i3.40
pages 285-299

SURFACE TEMPERATURE EFFECT ON FLOW NEAR THE DELTA WING AT THE REGIME OF STRONG INTERACTION

Georgiy Nikolaevich Dudin
Central Aerohydrodynamic Institute (TsAGI), 1, Zhukovsky Str., Zhukovsky, Moscow Region, 140180, Russian Federation
K. T. Myint
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia

SINOPSIS

The temperature effect on the flow characteristics and structure in a spatial boundary layer on a delta wing with sharp leading edges at hypersonic flight speeds is investigated. The regime of strong viscous-inviscid boundary-layer interaction with the external inviscid flow on a semi-infinite wing with an extension of the order of unity is considered. The change in the thickness of the wing in the transverse direction has a power character. The effect of the parameter characterizing the ratio of the wing thickness to the boundary-layer characteristic thickness on local characteristics of the flow and aerodynamic coefficients is studied. The results of numerical calculation of the boundary-layer flow characteristics both in the supercritical and the subcritical flow regions are presented.

REFERENCIAS

  1. Kozlova, I. G. and Mihaylov, V. V., Strong viscous interaction on a delta wing and a yawing.

  2. Dudin, G. N., Characteristics of the heat exchange on the surface of a delta wing in a hypersonic viscous gas flow.

  3. Neyland, V.Y., To the theory of the hypersonic flow interaction with the boundary layer for the separated two-dimensional and spatial flows, Part 1. Spatial flows.

  4. Dudin, G. N., Supercritical regimes of the hypersonic flow over a flat delta wing at the presence of the side slip angle.

  5. Heyz, U. D. and Probstin, R. F., Hypersonic Flow Theory.

  6. Dudin, G. N., Interaction of the hypersonic flow with the boundary layer on a thin delta.

  7. Chyornyy, G. G., Gas Flows with a High Supersonic Velocity.

  8. Bashkin, V A. and Dudin, G. N., Three-Dimensional Viscous Gas Flows.

  9. Dudin, G. N. and Lyjin, D. O., One method of the calculation of a strong viscous interaction on a delta wing.

  10. Neyland, V. Y., Bogolepov, V. V, Dudin, G. N., and Lipatov, I. I., Asymptotic Theory of Supersonic Viscous Gas Flows.

  11. Dudin, G. N., To the problem on self-similar solutions existence in the supersonic region at the hypersonic flow over a delta wing.


Articles with similar content:

RADIATING LAMINAR BOUNDARY LAYER FLOW OVER A FLAT PLATE AT A LARGE FREE-STREAM MACH NUMBER
International Heat Transfer Conference 6, Vol.5, 1978, issue
K. Krishna Prasad, S. P. Venkateshan
INFLUENCE OF THE PLATE SURFACE TEMPERATURE ON THE PROPAGATION OF DISTURBANCES IN A HYPERSONIC FLOW
TsAGI Science Journal, Vol.49, 2018, issue 5
Georgiy Nikolaevich Dudin, Vladimir Yakovlevich Neyland
High-Turbulent Gas Screen in a Supersonic Nozzle
Heat Transfer Research, Vol.31, 2000, issue 6-8
Viktor I. Terekhov, V. P. Lebedev, V. V. Lemanov
EFFECT OF INJECTION FROM THE A WEDGE SURFACE ON THE PROPAGATION OF DISTURBANCES IN A HYPERSONIC FLOW
TsAGI Science Journal, Vol.50, 2019, issue 6
Georgiy Nikolaevich Dudin, Vladimir Yakovlevich Neyland
NONUNIQUENESS OF THE SOLUTION IN THE VICINITY OF THE PLANE OF SYMMETRY OF A DELTA WING IN A HYPERSONIC FLOWWITH STRONG INTERACTION
TsAGI Science Journal, Vol.46, 2015, issue 3
Georgiy Nikolaevich Dudin, Phon Hai Nguyen