Effects of second-approximation of boundary layer theory in three-dimensional flow over bodies with a large aspect ratio at small angles of incidence

E. A. Lipchinskii; G. A. Tirskii; S. V. Utyuzhnikov

doi:10.1007/BF02029831

Effects of second-approximation of boundary layer theory in three-dimensional flow over bodies with a large aspect ratio at small angles of incidence

E. A. Lipchinskii, G. A. Tirskii, S. V. Utyuzhnikov

Research output: Contribution to journal › Article › peer-review

Abstract

The influence of the second-approximation effects of laminar boundary layer theory on the heat transfer in three-dimensional hypersonic flow over blunt cones with a large aspect ratio is investigated numerically. © 1995 Plenum Publishing Corporation.

Original language	English
Pages (from-to)	204-209
Number of pages	5
Journal	Fluid Dynamics
Volume	30
Issue number	2
DOIs	https://doi.org/10.1007/BF02029831
Publication status	Published - Apr 1995

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@article{b755e67dfa3b43af972d5d2df64536bd,

title = "Effects of second-approximation of boundary layer theory in three-dimensional flow over bodies with a large aspect ratio at small angles of incidence",

abstract = "The influence of the second-approximation effects of laminar boundary layer theory on the heat transfer in three-dimensional hypersonic flow over blunt cones with a large aspect ratio is investigated numerically. {\textcopyright} 1995 Plenum Publishing Corporation.",

author = "Lipchinskii, {E. A.} and Tirskii, {G. A.} and Utyuzhnikov, {S. V.}",

year = "1995",

month = apr,

doi = "10.1007/BF02029831",

language = "English",

volume = "30",

pages = "204--209",

journal = "Fluid Dynamics",

issn = "1573-8507",

publisher = "Pleiades Publishing",

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T1 - Effects of second-approximation of boundary layer theory in three-dimensional flow over bodies with a large aspect ratio at small angles of incidence

AU - Lipchinskii, E. A.

AU - Tirskii, G. A.

AU - Utyuzhnikov, S. V.

PY - 1995/4

Y1 - 1995/4

N2 - The influence of the second-approximation effects of laminar boundary layer theory on the heat transfer in three-dimensional hypersonic flow over blunt cones with a large aspect ratio is investigated numerically. © 1995 Plenum Publishing Corporation.

AB - The influence of the second-approximation effects of laminar boundary layer theory on the heat transfer in three-dimensional hypersonic flow over blunt cones with a large aspect ratio is investigated numerically. © 1995 Plenum Publishing Corporation.

U2 - 10.1007/BF02029831

DO - 10.1007/BF02029831

M3 - Article

SN - 1573-8507

VL - 30

SP - 204

EP - 209

JO - Fluid Dynamics

JF - Fluid Dynamics

IS - 2

ER -

Effects of second-approximation of boundary layer theory in three-dimensional flow over bodies with a large aspect ratio at small angles of incidence

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