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Accession Number:
ADB806018
Title:
Aerodynamic Characteristics and Flap Loads of Perforated Double Split Flaps on a Rectangular NACA 23012 Airfoil
Corporate Author:
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Report Date:
1943-01-01
Descriptive Note:
Wartime rept.
Pages:
0068
Distribution Statement:
Approved for public release; distribution is unlimited.
File Size:
15.82MB