Experiments to study strain-gage load calibrations on a wing structure at elevated temperatures / | ORKG Ask

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Strain-gage bridge calibration and flight loads measurements on a low-aspect-ratio thin wing /

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Experimental investigation at mach number of 3.0 of the effects of thermal stress and buckling on the flutter of four-bay aluminum alloy panels with length-width ratios of 10 /

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Bohon, Herman L.
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Experimental investigation at mach number of 3.0 of the effects of thermal stress and buckling on the flutter of four-bay aluminum alloy panels with length-width ratios of 10 /

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United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Stresses and loads; Structures.Includes bibliog...