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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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