The Transverse Curvature Effect in Compressible Axially Symmetric Laminar Boundary-Layer Flow-Reference-Cited by-同舟云学术

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The Transverse Curvature Effect in Compressible Axially Symmetric Laminar Boundary-Layer Flow

Published:1956-03 Issue:3 Volume:23 Page:208-224
ISSN:1936-9956
Container-title:Journal of the Aeronautical Sciences
language:en
Short-container-title:Journal of the Aeronautical Sciences

Author:

PROBSTEIN RONALD F.¹,ELLIOTT DAVID²

Affiliation:

1. Brown University,

2. Princeton University,

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.3537

Reference48 articles.

1. t For a discussion of this point see, for example, p.381of reference 16.

2. Some Effects of Surface Curvature on Laminar Boundary-Layer Flow

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