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Accession Number:
AD0029785
Title:
Experimental Influence Coefficients for the Deflection of the Wing of a Full-Scale, Swept-Wing Bomber
Descriptive Note:
Research memo.
Corporate Author:
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Report Date:
1954-04-22
Pagination or Media Count:
29.0
Distribution Statement:
APPROVED FOR PUBLIC RELEASE