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Accession Number:
AD0091844
Title:
INVESTIGATION AT HIGH SUBSONIC SPEEDS OF THE EFFECT OF HORIZONTAL-TAIL LOCATION ON LONGITUDINAL AND LATERAL STABILITY CHARACTERISTICS OF A COMPLETE MODEL HAVING A SWEPTBACK WING IN A HIGH LOCATION
Descriptive Note:
Research memo.
Corporate Author:
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Report Date:
1956-04-18
Pagination or Media Count:
50.0
Distribution Statement:
APPROVED FOR PUBLIC RELEASE