Static longitudinal stability and control, and lateral characteristics of model were measured; modifications to model for reducing drag were forward fuselage additions and special wing bodies; components and changes investigated included empennage, wing tip body, wing fences, wing trailing edge flaps, horizontal tail settings, and wing dihedral angle.
Wind-tunnel investigation of transonic-transport configuration utilizing drag-reducing devices at mach numbers from 0.20 to 1.03
NASA -- Tech Note
1961
117 pages
Aufsatz (Zeitschrift)
Englisch
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