Simplified Laminar Boundary-Layer Calculations for Bodies of Revolution and Yawed Wings-Reference-Cited by-同舟云学术

Simplified Laminar Boundary-Layer Calculations for Bodies of Revolution and Yawed Wings

Published:1952-08 Issue:8 Volume:19 Page:553-565
ISSN:1936-9956
Container-title:Journal of the Aeronautical Sciences
language:en
Short-container-title:Journal of the Aeronautical Sciences

Author:

ROTT NICHOLAS¹,CRABTREE L. F.¹

Affiliation:

1. Cornell University,

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.2381

Reference53 articles.

1. w h e r e / >! e distance of a point on the surface from the axis and x is again the arc length along the surface. (See, eg Schlichting,8p.204.) T h e boundary condition [Eq. (1.3)] remains unchanged. M a k i n g the same simplifying assumption about the existence of a one-parameter family of velocity profiles, the argu

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