Flight-Test Evaluation of the Longitudinal Stability and Control Characteristics of 0.5-Scale Models of the Fairchild Lark Pilotless-Aircraft Configuration. Static Longitudinal Stability of Models with Wing Flap Deflections of 0 Deg and 15 Deg, TED No. NACA 2387

Author: Stone, David G.
Year: 1947
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L6L17a
Link: https://digital.library.unt.edu/ark:/67531/metadc64202/

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