Official performance test of Douglas XO-2 equipped with Liberty '12' engine and standard steel propeller set at 18° (flying section report)
United States. Army. Air Service. Engineering Division.
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DescriptionThis document describes the Douglas XO-2 airplane and gives the results of flight performance tests, including observations made by the test pilots related to taxiing, landing, balance, stability, maneuverability, aileron control, rudder control, elevator control, banking, accessibility, and visibility. Also included are drawings showing the biplane from three different angles.
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