Wind tunnel tests at mach numbers up to 1.8 on a model with .03 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188)

Wind tunnel tests at mach numbers up to 1.8 on a model with .03 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188)

E.P. Sutton; P.G. Hutton; L.C. Squire
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/811
Date: 1965

Show full item record

Files in this item

Thumbnail
Name: arc-cp-0798.pdf
Size: 5.955Mb
Format: PDF
View/Open

This item appears in the following Collection(s)

Search AERADE


Browse

My Account