Free-flight Tests of 45 Deg Swept Wings of Aspect Ratio 3.15 and Taper Ratio 0.54 to Measure Wing Damping of the First Bending Mode and to Investigate the Possibility of Flutter at Transonic Speeds

Author: O'Kelly, Burke R.
Additional Authors: Lundstrom, Reginald R.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L54C22
Link: https://digital.library.unt.edu/ark:/67531/metadc52896/

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