Title: Wing-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an All-movable Triangular Wing of Aspect Ratio 4 Alone and with a Body
Abstract: Report presenting the aerodynamic characteristics of an all-movable, triangular-plan-form wing alone and with a body as determined from semispan model tests. The agreement between calculated and experimental results was not satisfactory for the most part, which seemed to be due to the failure of linear theory to define the actual flow field about the configurations investigated. Results regarding lift characteristics, drag characteristics, and pitching-moment characteristics are provided.
Publication Year: 1950
Publication Date: 1950-02-02
Language: en
Type: article
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Cited By Count: 3
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