Buckling analysis for axially compressed flat plates, structural sections, and stiffened plates reinforced with laminated composites /

Buckling tests of two integrally stiffened cylinders subjected to bending /

Anderson, James Kent.
Peterson, James P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1975

Prepared at Langley Research Center.N 71-28116.Includes bibliographical references (p. 9).Mode of ac...

Buckling of simply supported plywood plates under combined edgewise bending and compression /

Zahn, John J., 1932-
Romstad, Karl

"December 1965."Title from cover.Includes bibliographical references.Mode of access: Internet

Analysis of bonded joints /

Srinivas, S.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29).Mode of ...

Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads /

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

January 1973

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

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...

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 ...

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...

An approximate buckling analysis for rectangular orthotropic plates with centrally located cutouts /

Nemeth, Michael P.
Johnson, Eric R.
Stein, Manuel.
Langley Research Center.

January 1986

Prepared at Langley Research Center."February 1986"--Cover.Includes bibliographical references (p. 9...

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 tests of three 4.6 meter diameter aluminum honeycomb sandwich conical shells loaded under external pressure /

Anderson, James Kent.
Davis, Randall C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Minimum-weight designs for hat-stiffened composite panels under uniaxial compression /

Agarwal, Banarsi.
Davis, Randall C.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode ...

Advanced beaded and tubular structural panels /

Musgrove, Max D. (Max Donnell)
Greene, Bruce E.
Langley Research Center.
Boeing Aerospace Company.

"Prepared by the Boeing [Aerospace] Company ... for Langley Research Center.""September 1975."Cover ...

An elastoplastic analysis of a uniaxially loaded sheet with an interference-fit bolt /

Crews, John H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

Thermal-structural combined loads design criteria study /

Deriugin, V.
Langley Research Center.
Boeing Company.

January 1972

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 273-27...

Shear-flexible finite-element models of laminated composite plates and shells /

Noor, Ahmed Khairy, 1938-
Mathers, Michael D. (Michael Douglas)
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 42-45).Mode ...

Buckling tests of two integrally stiffened cylinders subjected to bending /

Anderson, James Kent.
Peterson, James P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1975

Prepared at Langley Research Center.N 71-28116.Includes bibliographical references (p. 9).Mode of ac...

Buckling of simply supported plywood plates under combined edgewise bending and compression /

Zahn, John J., 1932-
Romstad, Karl

"December 1965."Title from cover.Includes bibliographical references.Mode of access: Internet

Analysis of bonded joints /

Srinivas, S.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29).Mode of ...

Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads /

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

January 1973

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

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...

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 ...

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...

An approximate buckling analysis for rectangular orthotropic plates with centrally located cutouts /

Nemeth, Michael P.
Johnson, Eric R.
Stein, Manuel.
Langley Research Center.

January 1986

Prepared at Langley Research Center."February 1986"--Cover.Includes bibliographical references (p. 9...

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 tests of three 4.6 meter diameter aluminum honeycomb sandwich conical shells loaded under external pressure /

Anderson, James Kent.
Davis, Randall C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Minimum-weight designs for hat-stiffened composite panels under uniaxial compression /

Agarwal, Banarsi.
Davis, Randall C.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode ...

Advanced beaded and tubular structural panels /

Musgrove, Max D. (Max Donnell)
Greene, Bruce E.
Langley Research Center.
Boeing Aerospace Company.

"Prepared by the Boeing [Aerospace] Company ... for Langley Research Center.""September 1975."Cover ...

An elastoplastic analysis of a uniaxially loaded sheet with an interference-fit bolt /

Crews, John H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

Thermal-structural combined loads design criteria study /

Deriugin, V.
Langley Research Center.
Boeing Company.

January 1972

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 273-27...

Shear-flexible finite-element models of laminated composite plates and shells /

Noor, Ahmed Khairy, 1938-
Mathers, Michael D. (Michael Douglas)
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 42-45).Mode ...

Buckling tests of two integrally stiffened cylinders subjected to bending /

Anderson, James Kent.
Peterson, James P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1975

Prepared at Langley Research Center.N 71-28116.Includes bibliographical references (p. 9).Mode of ac...

Buckling of simply supported plywood plates under combined edgewise bending and compression /

Zahn, John J., 1932-
Romstad, Karl

"December 1965."Title from cover.Includes bibliographical references.Mode of access: Internet

Analysis of bonded joints /

Srinivas, S.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29).Mode of ...

Buckling analysis for axially compressed flat plates, structural sections, and stiffened plates reinforced with laminated composites /

Abstract

Extracted data

Buckling analysis for axially compressed flat plates, structural sections, and stiffened plates reinforced with laminated composites /

Abstract

Extracted data

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