Catalog Record: Experimental studies of flutter of buckled rectangular panels at mach numbers from 1.2 to 3.0 including effects of pressure differential and of panel width-length ratio | HathiTrust Digital Library

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Experimental studies of flutter of buckled rectangular panels at mach numbers from 1.2 to 3.0 including effects of pressure differential and of panel width-length ratio /
by Maurice A. Sylvester.

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Main Author: Sylvester, Maurice A.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration : [1961.
Subjects: Stresses and loads.
Note: Cover title.
"MAy 1961."
Stresses and loads.
Supersedes NACA RM L55I30.
Physical Description: 37 p. : ill. ; 26 cm.
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