Flight-Test Evaluation of the Longitudinal Stability and Control Characteristics of 0.5-Scale Models of the Fairchild Lark Pilotless-Aircraft Configuration. Standard Configuration with Wing Flaps Deflected 60 deg and Model Having Tail in Line with Wings. TED No. NACA 2387
1947
32 pages
Report
No indication
English
Aircraft fuselage configuration with upwardly deflected rear fuselage
European Patent Office | 2023
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