Investigation of the flow field on the expansion side of a delta wing with supersonic leading edges

Report (1965)
Faculty
Aerospace Engineering (Aerospace Engineering) (TU Delft)
Copyright: © 1965 Delft University of Technology
More Info
expand_more

Published Date

1965

Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Source:

Technische Hogeschool Delft, Vliegtuigbouwkunde, Rapport VTH-128

Faculty

Aerospace Engineering

Files

VTH-128.pdf
(pdf | 0.681 Mb)