Details of the configurational development of a dispenser system are treated. The design was based on experience in dispenser development and on preliminary investigations, taking into account geometrical compatibility requirements. The different investigated fin forms are presented. The aerodynamic stability behavior of the investigated fuselage-wing-fin configurations is discussed.
Aerodynamische Gesichtspunkte der Konfigurativen Systemauslegung Eines Dispensers (Aerodynamic Aspects of the Configurational Systems Layout of a Dispenser)
1987
4 pages
Report
No indication
English
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