Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span equal to 1

Author: Rainey, Robert W
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L9L30
Link: https://digital.library.unt.edu/ark:/67531/metadc58609/

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