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Some Effects of Aeroelasticity at Mach Numbers from 0.7 to 1.6 on the Rolling Effectiveness of Thin Flat-plate Delta Wings Having 45 Degree Swept Leading Edges and Full-span Constant-chord Ailerons

Authors :
Marley, Edward T
English, Roland D
Publication Year :
1952
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1952.

Details

Language :
English
Database :
NASA Technical Reports
Publication Type :
Report
Accession number :
edsnas.19930087937
Document Type :
Report

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