Studies in Panel Flutter at Higher Mach Numbers: I. Flat and Slightly Curved Panels at Mach number 2.81. II. Cylindrical Shells with Boundary Layer
<p>Part I.</p> <p>Two series of panel flutter tests were carried out in the Jet Propulsion Laboratory's 12 inch supersonic wind tunnel. Flat and slightly curved panels were tested at Mach number 2.81.</p> <p>The flat, rectangular panels were designed to study...
Internet
https://thesis.library.caltech.edu/5008/1/Anderson_wj_1963.pdfAnderson, William Judson (1963) Studies in Panel Flutter at Higher Mach Numbers: I. Flat and Slightly Curved Panels at Mach number 2.81. II. Cylindrical Shells with Boundary Layer. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/E3ZX-JG81. https://resolver.caltech.edu/CaltechETD:etd-12152005-081824 <https://resolver.caltech.edu/CaltechETD:etd-12152005-081824>