Studies of the Turbulent Boundary Layer on a Waisted Body of Revolution in Subsonic and Supersonic Flow

Studies of the Turbulent Boundary Layer on a Waisted Body of Revolution in Subsonic and Supersonic Flow
Author: K. G. Winter
Publsiher: Unknown
Total Pages: 76
Release: 1968
Genre: Electronic Book
ISBN: 0114703337

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Compressible Turbulent Boundary Layers

Compressible Turbulent Boundary Layers
Author: Anonim
Publsiher: Unknown
Total Pages: 580
Release: 1969
Genre: Compressibility
ISBN: UVA:X004374138

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NASA Technical Note

NASA Technical Note
Author: Anonim
Publsiher: Unknown
Total Pages: 492
Release: 1970
Genre: Electronic Book
ISBN: MINN:319510008462920

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Calculation of Skin Friction Intwo dimensional Transonic Turbulent Flow

Calculation of Skin Friction Intwo dimensional  Transonic  Turbulent Flow
Author: T. W. Swafford
Publsiher: Unknown
Total Pages: 54
Release: 1979
Genre: Boundary layer
ISBN: UOM:39015104959310

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author: Anonim
Publsiher: Unknown
Total Pages: 312
Release: 1971
Genre: Aeronautics
ISBN: UIUC:30112106623843

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NASA Technical Memorandum

NASA Technical Memorandum
Author: Anonim
Publsiher: Unknown
Total Pages: 108
Release: 1979
Genre: Aeronautics
ISBN: MINN:31951P00218779O

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Analysis of Turbulent Boundary Layers

Analysis of Turbulent Boundary Layers
Author: Tuncer Cebeci
Publsiher: Elsevier
Total Pages: 422
Release: 2012-12-02
Genre: Science
ISBN: 9780323151054

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Analysis of Turbulent Boundary Layers focuses on turbulent flows meeting the requirements for the boundary-layer or thin-shear-layer approximations. Its approach is devising relatively fundamental, and often subtle, empirical engineering correlations, which are then introduced into various forms of describing equations for final solution. After introducing the topic on turbulence, the book examines the conservation equations for compressible turbulent flows, boundary-layer equations, and general behavior of turbulent boundary layers. The latter chapters describe the CS method for calculating two-dimensional and axisymmetric laminar and turbulent boundary layers. This book will be useful to readers who have advanced knowledge in fluid mechanics, especially to engineers who study the important problems of design.

Some Turbulent Boundary layer Measurements Obtained from the Forebody of an Airplane at Mach Numbers Up to 1 72

Some Turbulent Boundary layer Measurements Obtained from the Forebody of an Airplane at Mach Numbers Up to 1 72
Author: Edwin J. Saltzman,David F. Fisher
Publsiher: Unknown
Total Pages: 52
Release: 1970
Genre: Skin friction (Aerodynamics)
ISBN: UIUC:30112106640615

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