Exploratory tests on a thin delta wing in the flow field of a rectangular foreplane at Mach number 1.8
1961
8 S., [3] Bl.
33 cm
graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
DDC: | 629.13432 |
MACH NUMBER EFFECTS ON VORTEX BREAKDOWN IN SUBSONIC FLOW OVER A DELTA WING
British Library Conference Proceedings | 2011
|Some exploratory jet flap tests on a 60-deg delta wing
SLUB | 1961
|Some exploratory jet-flap tests on a 60-deg delta wing
TIBKAT | 1961
|