A method for reducing the base drag of wings with blunt trailing edge
1972
S. 15 - 23
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
Unknown
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
|