Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing

Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing

M. D. Dobson
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/1135
Date: 1970

Show full item record

Files in this item

Thumbnail
Name: arc-cp-1122.pdf
Size: 1.322Mb
Format: PDF
View/Open

This item appears in the following Collection(s)

Search AERADE


Browse

My Account