An approximate method for calculating the laminar boundary layer on an infinite swept wing with arbitrary velocity and suction distributions

An approximate method for calculating the laminar boundary layer on an infinite swept wing with arbitrary velocity and suction distributions

A. W. Lindfield; H. G. Pinsent
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/529
Date: 1960

Show full item record

Files in this item

Thumbnail
Name: arc-cp-0516.pdf
Size: 2.181Mb
Format: PDF
View/Open

This item appears in the following Collection(s)

Search AERADE


Browse

My Account