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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