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Accession Number:
AD0256080
Title:
TRANSONIC INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF A SWEPT-WING FIGHTER-AIRPLANE MODEL WITH LEADING-EDGE DROOP IN COMBINATION WITH OUTBOARD CHORD-EXTENSIONS AND NOTCHES
Descriptive Note:
Corporate Author:
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C
Report Date:
1961-05-01
Pagination or Media Count:
1.0
Distribution Statement:
APPROVED FOR PUBLIC RELEASE