An Investigation of Four Wings of Square Plan Form at a Mach Number of 6.86 in the Langley 11-Inch Hypersonic Tunnel

Author: McLellan, Charles H.
Additional Authors: Bertram, Mitchel H.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51D17
Link: https://digital.library.unt.edu/ark:/67531/metadc58952/

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