The dynamic lateral control characteristics of airplane models having unswept wings with round-and sharp-leading-edge sections

James L. Hassell, Charles V. Bennett
naca-tn-2219
Nov 1950


An investigation has been conducted in the Langley free-flight tunnel for the purpose of comparing the dynamic lateral control characteristics of airplane models with round- and sharp-leading-edge wing sections. The two dynamic models used in the investigation had different mass characteristics.

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