Skin-Friction and Heat-Transfer Characteristics of a Laminar Boundary Layer on a Cylinder in Axial Incompressible Flow-Reference-Cited by-同舟云学术

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Skin-Friction and Heat-Transfer Characteristics of a Laminar Boundary Layer on a Cylinder in Axial Incompressible Flow

Published:1951-10 Issue:10 Volume:18 Page:671-675
ISSN:1936-9956
Container-title:Journal of the Aeronautical Sciences
language:en
Short-container-title:Journal of the Aeronautical Sciences

Author:

SEBAN R. A.¹,BOND R.¹

Affiliation:

1. University of California, Berkeley

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.2076

Reference3 articles.

1. The laminar boundary layer in compressible flow

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2. Heat transfer phenomenon in a retarded boundary layer over a moving continuous cylinder;Journal of Physics A: Mathematical and Theoretical;2023-03-24

3. Boundary Layer Investigations for Primarily Axial Flow Over a Stationary and Transversely Oscillating Cylinder;Journal of Fluids Engineering;2023-03-24

4. Combined effects of surface sharpness and transverse curvature on thermal transport in separating flow region;Physica Scripta;2023-02-14

5. Analysis of laminar boundary-layer separation in retarded flow over bodies of revolution;Canadian Journal of Physics;2022-02

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