Maximum Altitude and Maximum Mach Number Obtained With the Modified Douglas D-558-II Research Airplane During Demonstration Flights

Author: Dahlen, Theodore E.
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L53B24
Link: https://digital.library.unt.edu/ark:/67531/metadc62197/

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