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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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