NDLI: Laminar heat exchange on sharp and blunt plates in a hypersonic air flow

Content Provider	Springer Nature Link
Author	Borovoi, V. Ya. Egorov, I. V. Skuratov, A. S. Struminskaya, I. V.
Copyright Year	2005
Abstract	The results of an experimental investigation and numerical simulation of heat exchange are given for sharp and blunt plates in a hypersonic air flow. The experiments were carried out in a Ludwig-type wind tunnel at hypersonic Mach numbers and a Reynolds number ReL which varied over the range from 0.24 ⋅ 106 to 1.31 ⋅ 106. The bluntness radius r was varied over the range from 0.008 mm (almost sharp plate) to 4 mm (the corresponding Reynolds numbers Rer from 15 to 4 ⋅ 104). The numerical simulation was carried out by solving the complete two-dimensional Navier-Stokes equations. The experimental data were correlated using the well-known viscous hypersonic interaction parameters.
Starting Page	148
Ending Page	158
Page Count	11
File Format	PDF
ISSN	00154628
Journal	Fluid Dynamics
Volume Number	40
Issue Number	1
e-ISSN	15738507
Language	English
Publisher	Kluwer Academic Publishers-Consultants Bureau
Publisher Date	2005-01-01
Publisher Place	New York
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	plate bluntness laminar boundary layer entropy layer heat exchange viscous interaction experiment numerical simulation Navier-Stokes equations Mechanics, Fluids, Thermodynamics Mechanics Fluids Engineering Fluid Dynamics
Content Type	Text
Resource Type	Article
Subject	Fluid Flow and Transfer Processes Physics and Astronomy Mechanical Engineering

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Laminar heat exchange on sharp and blunt plates in a hypersonic air flow