Dixon, Sidney C.
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]
/ Sidney C. Dixon, George E. Griffith and Herman L. Bohon
.- Washington, D. C.: National Aeronautics and Space Administration, 1961
.- 28p.
.- ( National Aeronautics and Space Administration (NASA)
Subject Headings:
Thermal stress;
Author Added Entry:
Griffith, George E.;
Bohon, Herman L.;