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" was published by Langley Research Center in 1989 - Hampton, Va and it has 25 pages.
“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
- Number of Pages: 25
- Publisher: Langley Research Center
- Publish Date: 1989
- Publish Location: Hampton, Va
“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 Specifications:
- Pagination: 25 p. :
Edition Identifiers:
- The Open Library ID: OL22344795M - OL9680829W
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