Supersonic wind tunnel tests on a 1/12th scale model of the bristol type 188 research aircraft part 1 M = 1.4 to 2.0 part 2 M = 2.0 to 2.7

Supersonic wind tunnel tests on a 1/12th scale model of the bristol type 188 research aircraft part 1 M = 1.4 to 2.0 part 2 M = 2.0 to 2.7

C. R. Taylor; T. A. Cook
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/831
Date: 1965

Show full item record

Files in this item

Thumbnail
Name: arc-cp-0818.pdf
Size: 18.78Mb
Format: PDF
View/Open

This item appears in the following Collection(s)

Search AERADE


Browse

My Account