Experimental investigation at mach number 3.0 of the effects of thermal stress and buckling on the flutter of four bay aluminium alloy panels with length width ratios of 10 [NASA TN D-921]
By: Dixon, Sidney C.
Contributor(s): Griffith, George E | Bohon, Herman L.
Material type:
BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Description: 28p.Subject(s): Thermal stress
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