Chordwise and Spanwise Loadings Measured at a Large Triangular Wing Having an Aspect Ratio of 2 and a Thin, Subsonic-type Airfoil Section
1950-03-13
Miscellaneous
No indication
English
Engineering Index Backfile | 1948
|Wing with trailing edge having spanwise-chordwise continuous deformation capability
European Patent Office | 2023
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