A method for reducing the base drag of wings with blunt trailing edge
1972
S. 15 - 23
Langzeitarchivierung durch Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Buch
Unbekannt
Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities
Engineering Index Backfile | 1952
|Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities
Engineering Index Backfile | 1952
|