Tests in the Ames 40- by 80-Foot Wind Tunnel of an Airplane Model With an Aspect Ratio 4 Triangular Wing and an All-Movable Horizontal Tail - High-Lift Devices and Lateral Controls
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Tests in the Ames 40- by 80-Foot Wind Tunnel of an Airplane Model With an Aspect Ratio 4 Triangular Wing and an All-Movable Horizontal Tail - High-Lift Devices and Lateral Controls, report, February 20, 1953; (https://digital.library.unt.edu/ark:/67531/metadc59454/: accessed April 25, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.