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  • Laminated thin shell structures subjected to free vibration in a hygrothermal environment [microform] / Pascal K. Gotsis and James D. Guptill .

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Large deformation behavior of long shallow cylindrical composite panels [microform] / Douglas M. Carper, Michael W. Hyer, and Eric R. Johnson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
    • 1991

  • Interlaminar stress analysis of dropped-ply laminated plates and shells by a mixed method [microform] / Peter N. Harrison, Eric R. Johnson, James H. Starnes.

    • Text
    • Blacksburg, Va. : Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Heat transfer measurements for Stirling machine cylinders [microform] / A.A. Kornhauser ... [et al.].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Compression strength of composite primary structural components [microform] : semiannual status report : performance period: May 1, 1994 to October 31, 1994 / Eric R. Johnson, principal investigator.

    • Text
    • Blacksburg, Va. : Aerospace and Ocean Engineering Dept., Virginia Polytechnic and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1994

  • Completed Beltrami-Michell formulation for analyzing mixed boundary value problems in elasticity [microform] / Surya N. Patnaik ... [et al.].

    • Text
    • Cleveland, Ohio : Lewis Research Center, National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • The crack problem in a reinforced cylindrical shell [microform] / O. Selcuk Yahsi and F. Erdogan.

    • Text
    • Bethlehem, Penn. : Lehigh University ; [Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Vibration and structureborne noise in space station [microform] : progress report for NASA grant NAG-1-541 for the period January 1, 1986 - June 30, 1986 / prepared by Rimas Vaicaitis, principal investigator.

    • Text
    • [Washington, D.C.? : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, 1986?]
    • 1986

  • Vibrations and structureborne noise in space station [microform] : final report / R. Vaicaitis, C.S. Lyrintzis, and D.A. Bofilios.

    • Text
    • [Hampton, Va. : NASA Langley Reserach Center ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Load transfer in the stiffener-to-skin joints of a pressurized fuselage [microform] : NASA grant NAG-1-537, performance period, November 1, 1991 to April 30, 1995 / Eric R. Johnson, Naveen Rastogi.

    • Text
    • Blacksburg, Va. : College of Engineering, Virginia Polytechnic Institute and State University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, 1995]
    • 1995

  • The influence of lamination angles on the interior noise levels of an aircraft [microform] / Christian M. Fernholz, Jay H. Robinson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • LQR control of shell vibrations via piezoceramic actuators [microform] / R.C.H. del Rosario, R.C. Smith.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • LQR control of thin shell dynamics [microform] : formulation and numerical implementation / R.C.H. del Rosario and R.C. Smith.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • A study of failure in small pressurized cylindrical shells containing a crack [microform] / Craig A. Barwell, Lorenz Eber, and Ian M. Fyfe.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • A mixed multi-field finite element formulation for thermopiezoelectric composite shells [microform] / Ho-Jun Lee, Dimitris A. Saravanos.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects [microform] / by David Michael McGowan.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells [microform] : presented at the AIAA/ASCE/ASC 36th Structures, Structural Dynamics and Materials Conference, April 10-12, 1995, New Orleans, LA, Thermal Structures Category / Theodore F. Johnson, Michael F. Card.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A thermoelastic transversely isotropic thick walled cylinder/disk application [microform] : an analytical solution and study / S.M. Arnold.

    • Text
    • Cleveland, Ohio : Lewis Research Center ; Springfield, Va. : For sale by the National Technical Information Service, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58488

  • Segmented tubular cushion springs and spring assembly [microform].

    • Text
    • [Moffett Field, Calif. : NASA Ames Research Center, 1985]
    • 1985

  • Influence of an asymmetric ring on the modeling of an orthogonally stiffened cylindrical shell [microform] / Naveen Rastogi and Eric R. Johnson.

    • Text
    • Blacksburg, Va. : Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60750

  • Passive damping concepts for tubular beams with partial rotational and translational end restraints [microform] / by Zia Razzaq, David K. Muyundo.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65629

  • A cylindrical shell with a stress-free end which contains an axial part-through or through crack [microform] / F. Erdogan and O.S. Yahsi.

    • Text
    • Bethlehem, Pa. : Lehigh University ; [Washington, D.C. : National Aeronautics and Space Administration, 1983]
    • 1983

  • Transient thermal stresses in a reinforced hollow disk or cylinder containing a radial crack [microform] / by Renji Tang and F. Erdogan.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1983]
    • 1983

  • A pressurized cylindrical shell with a fixed end which contains an axial part-through or through crack [microform] / by O .S. Yahsi and F. Erdogan.

    • Text
    • Bethlehem, PA : Lehigh University ; [Washington, DC] : National Aeronautics and Space Administration, [1983]
    • 1983

  • Stress intensity factors in a reinforced thick-walled cylinder [microform] / Renji Tang and F. Erdogan.

    • Text
    • Bethlehem, Pa. : Lehigh University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • The modeling of piezoceramic patch interactions with shells, plates and beams [microform] / H.T. Banks, R.C. Smith.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Institute for Computer Applications in Science and Engineering, Langley Research Center, [1992]
    • 1992
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97953

  • An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders / Michael P. Nemeth.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo45682

  • The influence of lamination angles on the interior noise levels of an aircraft / Christian M. Fernholz, Jay H. Robinson.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 1996.
    • 1996-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67749

  • Buckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02 : test dates: 3-6 February 2009 / Mark W. Hilburger [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2017.
    • 2017-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82549

  • The exact solution for linear thermoelastic axisymmetric deformations of generally laminated circular cylindrical shells / Michael P. Nemeth and Marc R. Schultz.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33345

  • Forced vibrations of a visco-elastic cylinder case-bonded to a thin elastic shell.

    • Text
    • 1963.
    • 1963
    • 2 Items
    FormatCall NumberItem Location
    Text QA935 .H39Off-site
    FormatCall NumberItem Location
    Text FC65-7368Off-site

  • Buckling of structures : Symposium, Cambridge/USA, June 17-21, 1974 / editor, Bernard Budiansky.

    • Text
    • Berlin ; New York : Springer-Verlag, 1976.
    • 1976
    • 1 Item
    FormatCall NumberItem Location
    Text TA656.2.S95 1974Off-site

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