Postbuckling response of long thick isotropic plates loaded in compression including higher order transverse shearing effects /

Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage /

Jegley, Dawn C.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Experimental behavior of graphite-epoxy Y-stiffened specimens loaded in compression /

Sydow, P. Daniel.
Shuart, Mark J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Compressive buckling analysis of hat-stiffened panel /

Ko, William L.
Jackson, Raymond H.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 9.Mode of access: Internet

Buckling and postbuckling behavior of square compression-loaded graphite-expoxy plates with circular cutouts /

Nemeth, Michael P.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 13.Mode of access: Internet

Modal interaction in postbuckled plates : theory /

Thurston, Gaylen A.
Langley Research Center.

January 1989

Research performed at Langley Research Center.Bibliography: p. 17.Mode of access: Internet

Buckling behavior of long symmetrically laminated plates subjected to combined loadings /

Nemeth, Michael P.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 11-12).Mode of access: I...

Application of Newton's method to postbuckling of rings under pressure loadings /

Thurston, Gaylen A.
Langley Research Center.

January 1989

Research performed at Langley Research Center.Bibliography: p. 21.Mode of access: Internet

A solution procedure for behavior of thick plates on a nonlinear foundation and postbuckling behavior of long plates /

Stein, Manuel.
Stein, Peter A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 39.Distributed to depository libraries in microfiche."September 1983"--Cover.Includ...

An improved transverse shear deformation theory for laminated anisotropic plates /

Murthy, M. V. V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Analysis and testing of axial compression in imperfect slender truss struts /

Lake, Mark S.
Georgiadis, Nicholas, 1925-2001.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Numerical analysis and parametric studies of the buckling of composite orthotropic compression and shear panels /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 67-68).Mode ...

Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet /

Bigelow, C. A.
Langley Research Center.

January 1986

Prepared at Langley Research Center."January 1986."Includes bibliographical references (p. 11).Mode ...

Elastic stability of laminated, flat and curved, long rectangular plates subjected to combined inplane loads /

Viswanathan, A. V.
Baker, L. L.
Tamekuni, M.
Langley Research Center.
Boeing Commercial Airplane Company.

January 1974

"Prepared by the Boeing Commercial Airplane Company ... for Langley Research Center."Cover title.Bib...

Buckling loads of stiffened panels subjected to combined longitudinal compression and shear : results obtained with PASCO, EAL, and STAGS computer programs /

Stroud, W. Jefferson
Anderson, Melvin S.
Greene, William H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

Subject category 39.Distributed to depository libraries in microfiche."January 1984"--Cover.Includes...

Postbuckling response of long thick isotropic plates loaded in compression including higher order transverse shearing effects

Librescu, Liviu
Stein, Manuel
Sydow, P. Daniel

September 1990

Buckling and postbuckling results for aluminum plates loaded in compression are presented. The buckl...

Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage /

Jegley, Dawn C.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Experimental behavior of graphite-epoxy Y-stiffened specimens loaded in compression /

Sydow, P. Daniel.
Shuart, Mark J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Compressive buckling analysis of hat-stiffened panel /

Ko, William L.
Jackson, Raymond H.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 9.Mode of access: Internet

Buckling and postbuckling behavior of square compression-loaded graphite-expoxy plates with circular cutouts /

Nemeth, Michael P.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 13.Mode of access: Internet

Modal interaction in postbuckled plates : theory /

Thurston, Gaylen A.
Langley Research Center.

January 1989

Research performed at Langley Research Center.Bibliography: p. 17.Mode of access: Internet

Buckling behavior of long symmetrically laminated plates subjected to combined loadings /

Nemeth, Michael P.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 11-12).Mode of access: I...

Application of Newton's method to postbuckling of rings under pressure loadings /

Thurston, Gaylen A.
Langley Research Center.

January 1989

Research performed at Langley Research Center.Bibliography: p. 21.Mode of access: Internet

A solution procedure for behavior of thick plates on a nonlinear foundation and postbuckling behavior of long plates /

Stein, Manuel.
Stein, Peter A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 39.Distributed to depository libraries in microfiche."September 1983"--Cover.Includ...

An improved transverse shear deformation theory for laminated anisotropic plates /

Murthy, M. V. V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Analysis and testing of axial compression in imperfect slender truss struts /

Lake, Mark S.
Georgiadis, Nicholas, 1925-2001.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Numerical analysis and parametric studies of the buckling of composite orthotropic compression and shear panels /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 67-68).Mode ...

Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet /

Bigelow, C. A.
Langley Research Center.

January 1986

Prepared at Langley Research Center."January 1986."Includes bibliographical references (p. 11).Mode ...

Elastic stability of laminated, flat and curved, long rectangular plates subjected to combined inplane loads /

Viswanathan, A. V.
Baker, L. L.
Tamekuni, M.
Langley Research Center.
Boeing Commercial Airplane Company.

January 1974

"Prepared by the Boeing Commercial Airplane Company ... for Langley Research Center."Cover title.Bib...

Buckling loads of stiffened panels subjected to combined longitudinal compression and shear : results obtained with PASCO, EAL, and STAGS computer programs /

Stroud, W. Jefferson
Anderson, Melvin S.
Greene, William H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

Subject category 39.Distributed to depository libraries in microfiche."January 1984"--Cover.Includes...

Postbuckling response of long thick isotropic plates loaded in compression including higher order transverse shearing effects

Librescu, Liviu
Stein, Manuel
Sydow, P. Daniel

September 1990

Buckling and postbuckling results for aluminum plates loaded in compression are presented. The buckl...

Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage /

Jegley, Dawn C.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Experimental behavior of graphite-epoxy Y-stiffened specimens loaded in compression /

Sydow, P. Daniel.
Shuart, Mark J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Compressive buckling analysis of hat-stiffened panel /

Ko, William L.
Jackson, Raymond H.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 9.Mode of access: Internet

Postbuckling response of long thick isotropic plates loaded in compression including higher order transverse shearing effects /

Abstract

Extracted data

Postbuckling response of long thick isotropic plates loaded in compression including higher order transverse shearing effects /

Abstract

Extracted data

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