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Free-Flight Tests of 0.11-Scale North American F-100 Airplane Wings to Investigate the Possibility of Flutter in Transonic Speed Range at Varying Angles of Attack
Author:
O'Kelly, Burke R.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-SL54G29
Link:
https://digital.library.unt.edu/ark:/67531/metadc65286/
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