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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Stability Results Obtained with Douglas D-558-1 Airplane (BuAero No. 37971) in Flight Up to a Mach Number of 0.89
Language: en
Pages: 16
Flight Measurement of the Stability Characteristics of the Douglas D-558-1 Airplane (Buaero No. 37971) in Sideslips
Language: en
Pages: 28
Authors: Walter C. Williams
Categories: Douglas airplanes
Type: BOOK - Published: 1949 - Publisher:

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Measurement of the Dynamic Lateral Stability of the Douglas D-558-1 Airplane (BUAERO No. 37971) in Rudder Kicks at a Mach Number of 0.72
Language: en
Pages: 10
Authors: Hubert M. Drake
Categories: Airplanes
Type: BOOK - Published: 1949 - Publisher:

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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
Flight Investigation of the Longitudinal Stability and Control Characteristics of the Douglas D-558-I Airplane (BuAero No. 37972) at Mach Numbers Up to 0.89
Language: en
Pages: 26
Authors: Melvin Sadoff
Categories: Airplanes
Type: BOOK - Published: 1951 - Publisher:

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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
Measured Characteristics of the Douglas D-558-1 Airplane (BUAERO NO. 37971) in Two Landings
Language: en
Pages: 8
Authors: Hubert M. Drake
Categories: Airplanes
Type: BOOK - Published: 1949 - Publisher:

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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