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Портал Begell Электронная Бибилиотека e-Книги Журналы Справочники и Сборники статей Коллекции
Journal of Flow Visualization and Image Processing
SJR: 0.11 SNIP: 0.312 CiteScore™: 0.1

ISSN Печать: 1065-3090
ISSN Онлайн: 1940-4336

Выпуски:
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Journal of Flow Visualization and Image Processing

DOI: 10.1615/JFlowVisImageProc.2012004662
pages 113-120

NUMERICAL VISUALIZATION OF FLOW AROUND A SUPERSONIC FLYING VEHICLE WITH A CONICAL STABILIZER

Alexander N. Kravtsov
Central Aerohydrodynamic Institute named after Prof. N.Ye. Zhukovsky (TsAGI)
V. Yu. Lunin
Central Aerohydrodynamic Institute (TsAGI), 1 Zhukovsky Str., Zhukovsky, Moscow Region, 140180, Russian Federation
Tatiana Yurievna Melnichuk
Central Aerohydrodynamic Institute (TsAGI), Zhukovsky Str. 1, Zhukovsky, 140180, Russia

Краткое описание

The paper presents numerical research of supersonic flow around the aerodynamic configuration with a conical stabilizer (flare). Analysis of flow fields and distributions of the gas-dynamic parameters was carried out. The calculated results and the experimental data are compared. A characteristic feature is revealed which is associated with the nonmonotonic character of pressure distribution on the flare.

ЛИТЕРАТУРА

  1. Coleman, G. T. , A Study of Hypersonic Boundary Layers over a Family of Axisymmetric Bodies at Zero Incidence.

  2. Glotov, G. F. , Aerothermodynamics of Flying Vehicles in Photographs.

  3. Krasilshchikov, A. P. and Guryashkin, L. P. , Experimental Studies of Bodies of Revolution in Hypersonic Flows.

  4. Zhilin, Yu. L and Kovalenko, V. V. , On the binding of near and far fields in the problem of sonic boom.


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