Use of a wind tunnel to determine the performance of slender wings suitable for a supersonic transport aircraft

Use of a wind tunnel to determine the performance of slender wings suitable for a supersonic transport aircraft

J. Y. G. Evans
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/755
Date: 1964

Show full item record

Files in this item

Thumbnail
Name: arc-cp-0742.pdf
Size: 1.204Mb
Format: PDF
View/Open

This item appears in the following Collection(s)

Search AERADE


Browse

My Account