Effect of wing loading and altitude on lateral stability and control characteristics of an airplane as determined by tests of a model in the free-flight tunnel

Author: Campbell, John P.
Year: 1943
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-522, NACA-ARR-3F25
Link: https://digital.library.unt.edu/ark:/67531/metadc61008/

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