01516cam a2200349 a 4500011431962MiAaHDL20141013010000.0m d cr bn ---auaua841129s1984 dcua tb f00010 eng dsdr-uiuc682070ACU-8583(OCoLC)11434023GPOGPOUIU830-H-14 (microfiche)NAS 1.26:3815Simonds, R. A.Residual strength of five boron/aluminum laminates with crack-like notches after fatigue loading /R.A. Simonds ; prepared for Langley Research Center.Washington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Branch ;[Springfield, Va. :For sale by the National Technical Information Service],1984.35 p. :ill. ;28 cm.NASA contractor report ;3815Subject category 24."July 1984"--Cover.Distributed to depository libraries in microfiche."Virginia Polytechnic Institute and State University."Includes bibliographical references.Final report-task 3.NAS1-17100.Mode of access: Internet.AluminumFatigueMetalsFatigueBoronUnited States.National Aeronautics and Space Administration.Scientific and Technical Information Branch.Virginia Polytechnic Institute and State University.Langley Research Center.01143196220020415161639.020141013010000.020141112173021.02024-08-27T18:18:42ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc682070uiugSDRUIUCuiug.30112106737205UIU682070UIUUIUC20240827googleuiug.301121067372051984pdbibUS fed doc--NTIS: pubdate < 2020