Publication Date:
2019-07-12
Description:
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.
Keywords:
Aircraft Design, Testing and Performance
Type:
NACA-RM-SA7L04
Format:
application/pdf