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Experimental Investigation at Mach Number 3.0 of Effects of Thermal Stress and Buckling on Flutter Characteristics of Flat Single-bay Panels of Length-width Ration 0.96

Sidney C. Dixon

出版	National Aeronautics and Space Administration, 1962
URL	http://books.google.com.hk/books?id=UQh1AQAACAAJ&hl=&source=gbs_api