A new look at numerical analyses of free-edge stresses in composite laminates /

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...

Stress-concentration factors for finite orthotropic laminates with a circular hole and uniaxial loading /

Hong, C. S.
Crews, John H.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Includes statistical tables.Includes bibliographical references."May 1979"--Cover."Langley Research ...

An analysis of the relaxation of laminar boundary layer on a flat plate after passage of an interface with application to expansion-tube flows /

Gupta, Roop N.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 73-75).Mode ...

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 ...

Analysis of free-edge effects in composite laminates by an assumed-stress method.

Mandell, Gordon Keith

January 1970

Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1970. M.S.MICR...

Stress-concentration factors for finite orthotropic laminates with a pin-loaded hole /

Crews, John H.
Raju, I. S.
Hong, C. S.
Joint Institute for Advancement of Flight Sciences.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"May 1981"--Cover."The George Washington University Joint Institute for Advancement of Flight Scienc...

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 ...

A critical examination of stresses in an elastic single lap joint /

Cooper, Paul A.
Sawyer, James Wayne, 1941-
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

"September 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

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

Viswanathan, A. V.
Miller, R. E., Jr.
Soong, Tsai-Chen.
Langley Research Center.
Boeing Company.

January 1971

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Includes bibliographica...

Composite laminates, Interlaminar stresses at straight free edges of

Kassapoglou, Christos

January 1985

Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics; and, (M...

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...

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...

A method for determining local elastoplastic stress and strain in metallurgically bonded notched laminates subjected to a loading cycle /

Sova, J. A.
Crews, John H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Tensile stress-strain behavior of graphite/epoxy laminates /

Garber, D. P. (Donald P.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Kentron Technical Center.
Langley Research Center.

January 1982

"Kentron Technical Center.""August 1982"--Cover.Includes bibliographical references.Mode of access: ...

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:...

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...

Stress-concentration factors for finite orthotropic laminates with a circular hole and uniaxial loading /

Hong, C. S.
Crews, John H.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Includes statistical tables.Includes bibliographical references."May 1979"--Cover."Langley Research ...

An analysis of the relaxation of laminar boundary layer on a flat plate after passage of an interface with application to expansion-tube flows /

Gupta, Roop N.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 73-75).Mode ...

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 ...

Analysis of free-edge effects in composite laminates by an assumed-stress method.

Mandell, Gordon Keith

January 1970

Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1970. M.S.MICR...

Stress-concentration factors for finite orthotropic laminates with a pin-loaded hole /

Crews, John H.
Raju, I. S.
Hong, C. S.
Joint Institute for Advancement of Flight Sciences.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"May 1981"--Cover."The George Washington University Joint Institute for Advancement of Flight Scienc...

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 ...

A critical examination of stresses in an elastic single lap joint /

Cooper, Paul A.
Sawyer, James Wayne, 1941-
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

"September 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

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

Viswanathan, A. V.
Miller, R. E., Jr.
Soong, Tsai-Chen.
Langley Research Center.
Boeing Company.

January 1971

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Includes bibliographica...

Composite laminates, Interlaminar stresses at straight free edges of

Kassapoglou, Christos

January 1985

Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics; and, (M...

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...

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...

A method for determining local elastoplastic stress and strain in metallurgically bonded notched laminates subjected to a loading cycle /

Sova, J. A.
Crews, John H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Tensile stress-strain behavior of graphite/epoxy laminates /

Garber, D. P. (Donald P.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Kentron Technical Center.
Langley Research Center.

January 1982

"Kentron Technical Center.""August 1982"--Cover.Includes bibliographical references.Mode of access: ...

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:...

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...

Stress-concentration factors for finite orthotropic laminates with a circular hole and uniaxial loading /

Hong, C. S.
Crews, John H.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Includes statistical tables.Includes bibliographical references."May 1979"--Cover."Langley Research ...

An analysis of the relaxation of laminar boundary layer on a flat plate after passage of an interface with application to expansion-tube flows /

Gupta, Roop N.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 73-75).Mode ...

A new look at numerical analyses of free-edge stresses in composite laminates /

Abstract

Extracted data

A new look at numerical analyses of free-edge stresses in composite laminates /

Abstract

Extracted data

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