Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7 - Info and Reading Options
By Jose A. Rivera
“Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7” Metadata:
- Title: ➤ Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7
- Author: Jose A. Rivera
“Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7” Subjects and Themes:
- Subjects: Flutter analysis - Spanwise curvature
Edition Identifiers:
- The Open Library ID: OL9680829W
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