02080cam a2200457Ia 4500011429203MiAaHDL20141009010000.0m d cr bn ---auaua060505s1969 dcua bt f000 0 eng dsdr-uiuc6380757(OCoLC)68213455FERFERLHLUIUUNAS 1.26:1316NASA CR 1316Egle, D. M.A theoretical analysis of the free vibration of discretely stiffened cylindrical shells with arbitrary end conditions /by D.M. Egle and K.E. Soder.Washington, D.C. :National Aeronautics and Space Administration ;Springfield, Va. :For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor],1969.xi, 76 p. :ill. ;27 cm.NASA contractor report ;NASA CR-1316"NASA CR-1316.""June 1969"--Cover.Includes bibliographical references (p. 57-61).Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 11/15/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19690018786%5F1969018786.pdf.Prepared by University of Oklahoma, Norman, Okla. for Langley Research CenterNGR-37-003-035Mode of access: Internet.Vibration (Aeronautics)Cylindric algebras.Vibration effects.nasatStiffening.nasatFlexibility.nasatDigital computers.nasatComputer programs.nasatStiffness.nasatRayleigh-ritz method.nasatFree vibration.nasatCylindrical shells.nasatSoder, K. E.University of Oklahoma.Langley Research Center.United States.National Aeronautics and Space Administration.01142920320101022115225.020141009010000.020141112164151.02025-01-02T19:10:10Z2025-01-02T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6380757uiugSDRUIUCuiug.30112106856427UIU6380757UIUUIUC20250102googleuiug.301121068564271969pdbibUS fed doc