An experimental investigation of the characteristics of some plane and cambered 65° delta wings at mach numbers from 0.7 to 2.0
Report / Royal Aerospace Establishment ; AERO-2655
1961
30 S., 9 Taf., 53 Bl
Ill
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English