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Accession Number:
AD0006725
Title:
EFFECT OF LEADING-EDGE CHORD-EXTENSIONS ON THE AERODYNAMIC CHARACTERISTICS OF A 45 SWEPTBACK WING-FUSELAGE COMBINATION AT MACH NUMBERS OF 0.40 TO 1.03
Descriptive Note:
Reseach memo.
Corporate Author:
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Report Date:
1953-04-14
Pagination or Media Count:
43.0
Abstract:
Distribution Statement:
APPROVED FOR PUBLIC RELEASE