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Some Considerations Regarding the Application of the Supersonic Area Rule to the Design of Airplane Fuselages
Author:
Whitcomb, Richard T.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L56E23A
Link:
https://digital.library.unt.edu/ark:/67531/metadc53074/
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