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The Effect of Tip Tanks on the Rolling Characteristics at High Subsonic Mach Numbers of a Wing Having an Aspect Ratio of 3 with Quarter-chord Line Swept Back 35 Degrees

Authors :
Kuhn, Richard E
Myers, Boyd C , II
Publication Year :
1950
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1950.

Details

Language :
English
Database :
NASA Technical Reports
Publication Type :
Report
Accession number :
edsnas.19930086118
Document Type :
Report

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