01341cam a2200325Ia 4500011424856MiAaHDL20141013010000.0m d cr bn ---auaua910503s1991 dcua b f000 0 eng dsdr-uiuc6360069(OCoLC)23685816ABCABCOCLCQLHLUIUUNAS 1.15:4274TL521.3.T4A3 no. 4274Snyder, H. Todd.Determination of the effects of heating on modal characteristics of an aluminum plate with application to hypersonic vehicles /H. Todd Snyder, Michael W. Kehoe.Washington, D.C. :National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;Springfield, Va. :For sale by the National Technical Information Service,1991.24 p. :ill. ;28 cm.NASA technical memorandum ;4274Prepared at Dryden Flight Research Facility.Bibliography: p. 7.Mode of access: Internet.Hypersonic planesMaterialsTesting.Thermoelasticity.Modal analysis.VibrationTesting.High temperatures.Plates, AluminumHeating.Kehoe, M. W.Dryden Flight Research Facility.01142485620101004132521.020141013010000.020141112173021.02025-01-01T19:21:06Z2025-01-01T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6360069uiugSDRUIUCuiug.30112106612549UIU6360069UIUUIUC20250101googleuiug.301121066125491991pdbibUS fed doc--NTIS: pubdate < 2020