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Accession Number:
ADB805337
Title:
Considerations of the Total Drag of Supersonic Airfoil Sections
Descriptive Note:
Technical note
Corporate Author:
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Report Date:
1947-07-01
Pagination or Media Count:
26.0
Distribution Statement:
APPROVED FOR PUBLIC RELEASE
