Stability Results Obtained With Douglas D 558 1 Airplane Buaero No 37971 In Flight Up To A Mach Number Of 089
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In the course of a stability and control investigation of the D-558-1 airplane, rudder kicks were made at a Mach number of 0.72 at a pressure altitude of 8500 f
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Results and analysis pertaining to the longitudinal stability and control characteristics of the Douglas D558-1 airplane (BuAero No. 37972) are presented. The r
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Pages: 8
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Records were obtained of two landings of the Douglas D-558-1 airplane during the stability and control investigation. These two records show that the maximum no