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Flight Measurements of the Flying Qualities of a Lockheed P-80A Airplane (Army No. 44-85099) - Stalling Characteristics

Seth B. ANDERSON, George E. Cooper

Abstract

This report contains the flight-test results of the stalling characteristics measured during the flying-qualities investigation of the Lockheed P-8OA airplane (Army No. 44-85099). The tests were conducted in straight and turning flight with and without wing-tip tanks. These tests showed satisfactory stalling characteristics and adequate stall warning for all configurations and conditions tested.

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Available abstract

Key concepts: Airplane, Aeronautics, Engineering, Stall (fluid mechanics), Flight test, Aerospace engineering, Automotive engineering